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 28885U 26145.52163843 +.00000000 +00000-0 +00000-0 0 00004
2 28885 4.5861 76.1099 0003231 341.3756 59.7651 1.00280124 08
| Epoch (UTC): | 25 May 2026 12:31:09 |
| Eccentricity: | 0.0003231 |
| inclination: | 4.5861° |
| perigee height: | 35771 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 76.1099° |
| argument of perigee: | 341.3756° |
| revolutions per day: | 1.00280124 |
| mean anomaly at epoch: | 59.7651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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