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 23753U 26158.70280691 +.00000000 +00000-0 +39307-4 0 00004
2 23753 98.7056 229.3889 0004739 112.8049 247.3633 14.27029976 01
| Epoch (UTC): | 07 June 2026 16:52:02 |
| Eccentricity: | 0.0004739 |
| inclination: | 98.7056° |
| perigee height: | 798 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 229.3889° |
| argument of perigee: | 112.8049° |
| revolutions per day: | 14.27029976 |
| mean anomaly at epoch: | 247.3633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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