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 28899U 26121.40150030 +.00000000 +00000-0 +00000-0 0 00004
2 28899 5.0366 43.7577 0002941 0.3774 103.2003 1.00273450 09
| Epoch (UTC): | 01 May 2026 09:38:09 |
| Eccentricity: | 0.0002941 |
| inclination: | 5.0366° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 43.7577° |
| argument of perigee: | 0.3774° |
| revolutions per day: | 1.00273450 |
| mean anomaly at epoch: | 103.2003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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