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 03093U 26053.86052727 +.00000000 +00000-0 -44811-4 0 00004
2 03093 105.8038 259.9420 0319588 291.3330 82.6518 12.83599789 09
| Epoch (UTC): | 22 February 2026 20:39:09 |
| Eccentricity: | 0.0319588 |
| inclination: | 105.8038° |
| perigee height: | 1081 km |
| apogee height: | 1573 km |
| right ascension of ascending node: | 259.9420° |
| argument of perigee: | 291.3330° |
| revolutions per day: | 12.83599789 |
| mean anomaly at epoch: | 82.6518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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