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 28096U 26064.04805130 +.00000000 +00000-0 +10418-3 0 00004
2 28096 63.6798 298.0441 0073503 118.1213 242.7267 13.41062396 04
| Epoch (UTC): | 05 March 2026 01:09:11 |
| Eccentricity: | 0.0073503 |
| inclination: | 63.6798° |
| perigee height: | 1050 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 298.0441° |
| argument of perigee: | 118.1213° |
| revolutions per day: | 13.41062396 |
| mean anomaly at epoch: | 242.7267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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