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 04793U 26032.03185295 +.00000000 +00000-0 +12420-3 0 00004
2 04793 101.3584 72.6001 0031267 253.0216 173.1114 12.54048556 09
| Epoch (UTC): | 01 February 2026 00:45:52 |
| Eccentricity: | 0.0031267 |
| inclination: | 101.3584° |
| perigee height: | 1423 km |
| apogee height: | 1472 km |
| right ascension of ascending node: | 72.6001° |
| argument of perigee: | 253.0216° |
| revolutions per day: | 12.54048556 |
| mean anomaly at epoch: | 173.1114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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