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Deimos

In orbit NORAD 60526 IYTF-0254-0953-7251-9719

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

29

Observations all time

Mission information
Spacecraft name
Deimos
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
2024-08-16 18:56:00
Separation time
2024-08-16 19:52:26
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
416.10 km
Apogee
422.14 km
Inclination
97.4°
Period
93.0 min
Semi-major axis
6797.1 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:44 UTC
Two-line elements (TLE)
1 60526U 24149BL  26284.18831401  .00028375  00000-0  53980-3 0  9990
2 60526 97.3736 12.3417 0004489 207.1882 152.9134 15.48189808120377
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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
2026-10-12 15:37:06 STARLINK-1167
NORAD 45071
DEIMOS
NORAD 60526
2.211 8.71 2.3e-05
2026-10-15 18:09:46 DEIMOS
NORAD 60526
POLYTECH UNIVERSE-4
NORAD 61747
4.717 14.49 8.9e-08
2026-10-15 22:18:34 STARLINK-1368
NORAD 45540
DEIMOS
NORAD 60526
4.250 13.51 4.1e-06
2026-10-16 00:22:07 DEIMOS
NORAD 60526
OBJECT AU
NORAD 61777
1.632 14.47 7.5e-07
2026-10-16 05:32:50 STARLINK-2421
NORAD 48098
DEIMOS
NORAD 60526
0.136 14.79 3.0e-03
2026-10-17 07:54:41 STARLINK-1300
NORAD 45374
DEIMOS
NORAD 60526
3.980 14.80 3.5e-06

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