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 51812U 26145.27625118 +.00000000 +00000-0 +49014-4 0 00002
2 51812 53.2131 345.3074 0001169 98.8989 261.2136 15.08836545 04
| Epoch (UTC): | 25 May 2026 06:37:48 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 345.3074° |
| argument of perigee: | 98.8989° |
| revolutions per day: | 15.08836545 |
| mean anomaly at epoch: | 261.2136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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