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 29656U 26105.79443212 +.00000000 +00000-0 +00000-0 0 00007
2 29656 11.4453 39.7818 0004072 304.4404 279.2613 0.99008336 04
| Epoch (UTC): | 15 April 2026 19:03:58 |
| Eccentricity: | 0.0004072 |
| inclination: | 11.4453° |
| perigee height: | 36127 km |
| apogee height: | 36162 km |
| right ascension of ascending node: | 39.7818° |
| argument of perigee: | 304.4404° |
| revolutions per day: | 0.99008336 |
| mean anomaly at epoch: | 279.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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