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 23088U 26088.15518139 +.00000000 +00000-0 +20679-3 0 00008
2 23088 71.0019 30.0056 0005474 267.5988 92.4508 14.15015668 05
| Epoch (UTC): | 29 March 2026 03:43:27 |
| Eccentricity: | 0.0005474 |
| inclination: | 71.0019° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 30.0056° |
| argument of perigee: | 267.5988° |
| revolutions per day: | 14.15015668 |
| mean anomaly at epoch: | 92.4508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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