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LUNA-2

In orbit NORAD 68470 IMHH-4032-1798-6391-5710

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

59

Observations all time

Mission information
Spacecraft name
LUNA-2
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-30 11:02:00
Separation time
Last observers
Observer
Time of receipt
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
501.51 km
Apogee
512.62 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6885.2 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 68470U 26067BG  26284.14421227  .00006487  00000-0  31666-3 0  9991
2 68470 97.4622 240.6826 0008066 38.4740 321.7068 15.18592573 29522
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-13 08:47:27 XINGSHIDAI 20
NORAD 58918
LUNA-2
NORAD 68470
4.461 12.03 1.5e-07
2026-10-14 14:21:38 LUNA-2
NORAD 68470
FALCON 9 DEB
NORAD 48608
0.380 6.58 2.8e-05
2026-10-15 03:33:11 LUNA-2
NORAD 68470
PEGASUS DEB
NORAD 24980
2.821 15.12 1.9e-07
2026-10-15 04:16:13 MICE-1
NORAD 66684
LUNA-2
NORAD 68470
2.045 12.74 6.5e-07
2026-10-15 06:17:40 LUNA-2
NORAD 68470
COSMOS 2251 DEB
NORAD 36047
4.937 15.17 6.2e-08
2026-10-15 08:14:03 CARTOSAT-3
NORAD 44804
LUNA-2
NORAD 68470
3.922 11.80 2.0e-07
2026-10-15 11:11:33 OBJECT B
NORAD 65260
LUNA-2
NORAD 68470
3.172 15.01 1.6e-07
2026-10-15 14:21:24 OBJECT C
NORAD 65261
LUNA-2
NORAD 68470
3.214 15.00 1.6e-07
2026-10-15 15:56:12 OBJECT D
NORAD 65262
LUNA-2
NORAD 68470
4.432 15.01 8.2e-08
2026-10-16 15:19:11 LUNA-2
NORAD 68470
CZ-6A DEB
NORAD 60626
2.039 1.52 1.1e-06
2026-10-16 15:42:48 STARLINK-2112
NORAD 47391
LUNA-2
NORAD 68470
4.782 13.75 3.0e-06
2026-10-16 16:39:12 CARTOSAT-2D
NORAD 41948
LUNA-2
NORAD 68470
1.896 11.61 8.5e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite