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 26073.28375127 +.00000000 +00000-0 +48358-4 0 00003
2 28654 98.8150 154.3266 0015171 63.2958 296.9766 14.13711775 05
| Epoch (UTC): | 14 March 2026 06:48:36 |
| Eccentricity: | 0.0015171 |
| inclination: | 98.8150° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 154.3266° |
| argument of perigee: | 63.2958° |
| revolutions per day: | 14.13711775 |
| mean anomaly at epoch: | 296.9766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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