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MARMOTSat

In orbit NORAD 69912 HPYK-4830-8894-4849-3491 Canada

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

233

Observations all time

Mission information
Spacecraft name
MARMOTSat
Call sign
VA7UVS
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
2026-07-07 07:12:00
Separation time
2026-07-07 08:07:51
Last observers
Observer
Time of receipt
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
589.96 km
Apogee
593.69 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6970.0 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 69912U 26156AV  26284.18248435  .00001444  00000-0  15164-3 0  9997
2 69912 97.7455 182.9083 0002690 148.3148 211.8233 14.91003436 14289
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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
2026-10-11 22:26:17 MARMOTSAT
NORAD 69912
FENGYUN 1C DEB
NORAD 31087
4.098 13.04 1.5e-07
2026-10-12 15:01:43 AAC-AIS-SAT1
NORAD 55107
MARMOTSAT
NORAD 69912
2.919 14.98 1.9e-07
2026-10-13 08:16:57 LEMUR-2-GRAM-E-SUE
NORAD 67370
MARMOTSAT
NORAD 69912
4.734 11.32 1.4e-07
2026-10-13 12:15:34 MARMOTSAT
NORAD 69912
SL-14 R/B
NORAD 16327
4.251 5.49 5.4e-07
2026-10-14 13:10:59 MARMOTSAT
NORAD 69912
CZ-4B DEB
NORAD 39052
0.984 14.49 2.0e-06
2026-10-15 01:19:47 MARMOTSAT
NORAD 69912
COSMOS 2251 DEB
NORAD 36441
3.852 12.88 1.8e-07
2026-10-15 22:00:39 MARMOTSAT
NORAD 69912
TRISAT-S
NORAD 100612
3.492 14.95 1.3e-07
2026-10-16 01:13:55 MARMOTSAT
NORAD 69912
OBJECT A
NORAD 100609
4.480 14.95 7.9e-08
2026-10-16 02:23:53 MARMOTSAT
NORAD 69912
NOAA 16 DEB
NORAD 41520
1.341 10.61 1.8e-06
2026-10-17 03:07:10 MARMOTSAT
NORAD 69912
CZ-6A DEB
NORAD 54592
1.775 14.81 5.3e-07
2026-10-17 04:43:50 MARMOTSAT
NORAD 69912
CZ-6A DEB
NORAD 54592
4.559 14.81 8.1e-08
2026-10-17 13:53:39 MARMOTSAT
NORAD 69912
FENGYUN 1C DEB
NORAD 31768
1.807 14.12 6.4e-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