View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 51991U 26145.07844521 +.00000000 +00000-0 +28719-4 0 00008
2 51991 53.2136 56.1971 0001232 80.8465 279.2666 15.08843636 07
| Epoch (UTC): | 25 May 2026 01:52:57 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 56.1971° |
| argument of perigee: | 80.8465° |
| revolutions per day: | 15.08843636 |
| mean anomaly at epoch: | 279.2666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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