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 26161.60367279 +.00000000 +00000-0 +16404-3 0 00008
2 23088 70.9994 235.7573 0003196 193.0050 167.0991 14.15020786 07
| Epoch (UTC): | 10 June 2026 14:29:17 |
| Eccentricity: | 0.0003196 |
| inclination: | 70.9994° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 235.7573° |
| argument of perigee: | 193.0050° |
| revolutions per day: | 14.15020786 |
| mean anomaly at epoch: | 167.0991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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