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 28654U 26069.88653876 +.00000000 +00000-0 +54673-4 0 00001
2 28654 98.8154 150.9770 0015267 72.3092 287.9746 14.13711200 08
| Epoch (UTC): | 10 March 2026 21:16:36 |
| Eccentricity: | 0.0015267 |
| inclination: | 98.8154° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 150.9770° |
| argument of perigee: | 72.3092° |
| revolutions per day: | 14.13711200 |
| mean anomaly at epoch: | 287.9746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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