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 07490U 26088.11354256 +.00000000 +00000-0 +88133-4 0 00001
2 07490 81.1889 216.3475 0029262 309.1264 50.7306 14.10556092 05
| Epoch (UTC): | 29 March 2026 02:43:30 |
| Eccentricity: | 0.0029262 |
| inclination: | 81.1889° |
| perigee height: | 836 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 216.3475° |
| argument of perigee: | 309.1264° |
| revolutions per day: | 14.10556092 |
| mean anomaly at epoch: | 50.7306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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