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 28372U 26145.27481894 +.00000000 +00000-0 +60951-4 0 00001
2 28372 98.6309 155.3763 0043740 223.7524 136.0202 14.51764156 06
| Epoch (UTC): | 25 May 2026 06:35:44 |
| Eccentricity: | 0.0043740 |
| inclination: | 98.6309° |
| perigee height: | 689 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 155.3763° |
| argument of perigee: | 223.7524° |
| revolutions per day: | 14.51764156 |
| mean anomaly at epoch: | 136.0202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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