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 26162.48903742 +.00000000 +00000-0 +31104-4 0 00000
2 23753 98.7054 233.1573 0004805 104.0118 256.1597 14.27030602 01
| Epoch (UTC): | 11 June 2026 11:44:12 |
| Eccentricity: | 0.0004805 |
| inclination: | 98.7054° |
| perigee height: | 798 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 233.1573° |
| argument of perigee: | 104.0118° |
| revolutions per day: | 14.27030602 |
| mean anomaly at epoch: | 256.1597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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