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 26158.91739582 +.00000000 +00000-0 +11707-3 0 00009
2 23088 70.9995 241.3984 0003357 196.3267 163.7748 14.15019357 07
| Epoch (UTC): | 07 June 2026 22:01:02 |
| Eccentricity: | 0.0003357 |
| inclination: | 70.9995° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 241.3984° |
| argument of perigee: | 196.3267° |
| revolutions per day: | 14.15019357 |
| mean anomaly at epoch: | 163.7748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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