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 28375U 26100.16149208 +.00000000 +00000-0 +10229-3 0 00005
2 28375 98.6552 62.9399 0079452 322.7845 36.7853 14.43842295 02
| Epoch (UTC): | 10 April 2026 03:52:32 |
| Eccentricity: | 0.0079452 |
| inclination: | 98.6552° |
| perigee height: | 689 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 62.9399° |
| argument of perigee: | 322.7845° |
| revolutions per day: | 14.43842295 |
| mean anomaly at epoch: | 36.7853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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