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MR-2

In orbit NORAD 67556 ZADI-4461-1712-8089-8336 Spain

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2026

Launch

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Mission information
Spacecraft name
MR-2
Other names
2026-015A
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2026-01-22 00:00:00
Separation time
2026-01-22 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
1055.45 km
Apogee
1063.31 km
Inclination
89.0°
Period
106.5 min
Semi-major axis
7437.5 km
Velocity
7.32 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 67556U 26015A   26283.96691565  .00000049  00000-0  54958-4 0  9999
2 67556  88.9967 256.7816 0005284  98.0550 262.1202 13.52702335 35362
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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 18:17:24 MR-2
NORAD 67556 		QIANFAN-197
NORAD 69415 		4.071 1.45 2.7e-07
2026-10-11 18:19:24 MR-2
NORAD 67556 		COSMOS 1275 DEB
NORAD 13053 		0.456 9.17 1.7e-05
2026-10-12 18:06:40 MR-2
NORAD 67556 		THOR ABLESTAR R/B
NORAD 893 		4.078 14.64 3.7e-07
2026-10-12 19:53:02 MR-2
NORAD 67556 		THOR ABLESTAR R/B
NORAD 893 		2.229 14.64 1.3e-06
2026-10-12 21:39:25 MR-2
NORAD 67556 		THOR ABLESTAR R/B
NORAD 893 		1.909 14.64 1.7e-06
2026-10-12 23:25:47 MR-2
NORAD 67556 		THOR ABLESTAR R/B
NORAD 893 		3.591 14.64 4.8e-07
2026-10-13 04:07:27 QIANFAN-58
NORAD 62788 		MR-2
NORAD 67556 		2.626 14.59 2.2e-07
2026-10-13 05:54:02 QIANFAN-58
NORAD 62788 		MR-2
NORAD 67556 		0.712 14.59 2.9e-06
2026-10-13 07:40:37 QIANFAN-58
NORAD 62788 		MR-2
NORAD 67556 		3.186 14.59 1.5e-07
2026-10-13 12:55:05 MR-2
NORAD 67556 		QIANFAN-223
NORAD 69852 		4.387 14.25 9.0e-08
2026-10-14 02:15:11 MR-2
NORAD 67556 		TRANSAT
NORAD 10457 		4.008 14.61 9.4e-08
2026-10-14 04:54:59 MR-2
NORAD 67556 		THOR ABLESTAR R/B
NORAD 703 		3.752 14.58 4.5e-07
2026-10-14 05:03:58 MR-2
NORAD 67556 		COSMOS 886 DEB
NORAD 9798 		4.716 13.60 9.5e-08
2026-10-15 11:03:55 QIANFAN-108
NORAD 66050 		MR-2
NORAD 67556 		3.791 13.48 1.5e-07
2026-10-16 03:03:07 QIANFAN-30
NORAD 61563 		MR-2
NORAD 67556 		3.890 14.20 1.2e-07
2026-10-16 05:38:47 MR-2
NORAD 67556 		THORAD AGENA D DEB
NORAD 42516 		2.217 11.26 6.2e-07
2026-10-16 13:47:13 QIANFAN-56
NORAD 62786 		MR-2
NORAD 67556 		3.346 14.59 1.3e-07
2026-10-16 15:33:48 QIANFAN-56
NORAD 62786 		MR-2
NORAD 67556 		0.683 14.59 3.2e-06
2026-10-16 17:17:25 MR-2
NORAD 67556 		TRANSIT 5B-2 DEB
NORAD 25156 		1.444 14.58 7.1e-07
2026-10-16 17:20:23 QIANFAN-56
NORAD 62786 		MR-2
NORAD 67556 		2.426 14.59 2.5e-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