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 29092U 26065.52545997 +.00000000 +00000-0 +14971-3 0 00005
2 29092 97.7558 88.8309 0001468 93.5731 266.5654 14.87577481 04
| Epoch (UTC): | 06 March 2026 12:36:39 |
| Eccentricity: | 0.0001468 |
| inclination: | 97.7558° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 88.8309° |
| argument of perigee: | 93.5731° |
| revolutions per day: | 14.87577481 |
| mean anomaly at epoch: | 266.5654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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