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 26074.22887642 +.00000000 +00000-0 -54803-4 0 00007
2 23088 70.9985 59.2525 0005641 280.1567 79.8919 14.15010198 07
| Epoch (UTC): | 15 March 2026 05:29:34 |
| Eccentricity: | 0.0005641 |
| inclination: | 70.9985° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 59.2525° |
| argument of perigee: | 280.1567° |
| revolutions per day: | 14.15010198 |
| mean anomaly at epoch: | 79.8919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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