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 28893U 26145.57044123 +.00000000 +00000-0 +62085-4 0 00002
2 28893 98.2830 279.7634 0014122 352.4422 7.6565 14.64139456 04
| Epoch (UTC): | 25 May 2026 13:41:26 |
| Eccentricity: | 0.0014122 |
| inclination: | 98.2830° |
| perigee height: | 670 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 279.7634° |
| argument of perigee: | 352.4422° |
| revolutions per day: | 14.64139456 |
| mean anomaly at epoch: | 7.6565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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