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 26071.18912279 +.00000000 +00000-0 -88961-4 0 00006
2 23088 70.9985 65.6373 0005696 283.1836 76.8650 14.15010986 05
| Epoch (UTC): | 12 March 2026 04:32:20 |
| Eccentricity: | 0.0005696 |
| inclination: | 70.9985° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 65.6373° |
| argument of perigee: | 283.1836° |
| revolutions per day: | 14.15010986 |
| mean anomaly at epoch: | 76.8650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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