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 51798U 26145.05360690 +.00000000 +00000-0 -30242-4 0 00006
2 51798 53.2139 6.3082 0001218 95.7497 264.3634 15.08835084 07
| Epoch (UTC): | 25 May 2026 01:17:11 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 6.3082° |
| argument of perigee: | 95.7497° |
| revolutions per day: | 15.08835084 |
| mean anomaly at epoch: | 264.3634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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