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 28810U 26145.34270774 +.00000000 +00000-0 +31902-3 0 00002
2 28810 98.0112 268.2893 0019704 185.5407 174.5606 15.10647679 06
| Epoch (UTC): | 25 May 2026 08:13:29 |
| Eccentricity: | 0.0019704 |
| inclination: | 98.0112° |
| perigee height: | 521 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 268.2893° |
| argument of perigee: | 185.5407° |
| revolutions per day: | 15.10647679 |
| mean anomaly at epoch: | 174.5606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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