Chandrayan 2

 

Mission type	Lunar orbiter, lander, rover
Operator	Indian Space Research Organisation (ISRO)
COSPAR ID	2019-042A
SATCAT no.	44441
Website	www.isro.gov.in/chandrayaan2-home-0
Mission duration	Orbiter: ~ 7.5 years (planned); 1 year, 10 months, 1 day (elapsed) Vikram lander: ≤ 14 days (planned);[1][2] 0 days (landing failure) Pragyan rover: ≤ 14 days (planned);[2] 0 days (landing failure)
Spacecraft properties
Manufacturer	Indian Space Research Organisation (ISRO)
Launch mass	Combined (wet): 3,850 kg (8,490 lb) [3][4][5] Combined (dry): 1,308 kg (2,884 lb) [6] Orbiter (wet): 2,379 kg (5,245 lb) [4][5] Orbiter (dry): 682 kg (1,504 lb) [6] Vikram lander (wet): 1,471 kg (3,243 lb) [4][5] Vikram lander (dry): 626 kg (1,380 lb)[6] Pragyan rover: 27 kg (60 lb) [4][5]
Power	Orbiter: 1000 watts [7] Vikram lander: 650 watts [8] Pragyan rover: 50 watts
Start of mission
Launch date	22 July 2019, 09:13:12 UTC[9]
Rocket	GSLV Mark III M1 [10][11]
Launch site	Satish Dhawan Space Centre Second Launch Pad
Contractor	Indian Space Research Organisation (ISRO)
Moon orbiter
Orbital insertion	20 August 2019, 03:32 UTC [12][13]
Orbital parameters
Pericynthion altitude	100 km (62 mi) [14]
Apocynthion altitude	100 km (62 mi)
Moon lander
Spacecraft component	Rover
Landing date	6 September 2019, 20:23 UTC [13][15]
Landing site	Lunar south pole (intended)
Chandrayaan programme ← Chandrayaan-1 Chandrayaan-3 →