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 26069.13905764 +.00000000 +00000-0 -10093-3 0 00009
2 23088 70.9985 69.9432 0005717 285.2568 74.7922 14.15011712 04
| Epoch (UTC): | 10 March 2026 03:20:14 |
| Eccentricity: | 0.0005717 |
| inclination: | 70.9985° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 69.9432° |
| argument of perigee: | 285.2568° |
| revolutions per day: | 14.15011712 |
| mean anomaly at epoch: | 74.7922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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