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 26065.39239031 +.00000000 +00000-0 -69389-4 0 00003
2 23088 70.9986 77.8125 0005696 288.8436 71.2068 14.15012969 09
| Epoch (UTC): | 06 March 2026 09:25:02 |
| Eccentricity: | 0.0005696 |
| inclination: | 70.9986° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 77.8125° |
| argument of perigee: | 288.8436° |
| revolutions per day: | 14.15012969 |
| mean anomaly at epoch: | 71.2068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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