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 51803U 26145.31489145 +.00000000 +00000-0 +21548-4 0 00007
2 51803 53.2136 5.1345 0001150 98.6454 261.4668 15.08833241 08
| Epoch (UTC): | 25 May 2026 07:33:26 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 5.1345° |
| argument of perigee: | 98.6454° |
| revolutions per day: | 15.08833241 |
| mean anomaly at epoch: | 261.4668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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