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 26065.32477566 +.00000000 +00000-0 +00000-0 0 00008
2 28899 4.9598 43.8038 0002699 323.6854 56.9722 1.00271905 02
| Epoch (UTC): | 06 March 2026 07:47:40 |
| Eccentricity: | 0.0002699 |
| inclination: | 4.9598° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 43.8038° |
| argument of perigee: | 323.6854° |
| revolutions per day: | 1.00271905 |
| mean anomaly at epoch: | 56.9722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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