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 29108U 26085.96242534 +.00000000 +00000-0 +21522-3 0 00004
2 29108 98.4523 98.8150 0001423 110.6860 249.4497 14.69181259 01
| Epoch (UTC): | 26 March 2026 23:05:53 |
| Eccentricity: | 0.0001423 |
| inclination: | 98.4523° |
| perigee height: | 663 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 98.8150° |
| argument of perigee: | 110.6860° |
| revolutions per day: | 14.69181259 |
| mean anomaly at epoch: | 249.4497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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