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 23940U 26150.48520478 +.00000000 +00000-0 +19778-3 0 00008
2 23940 98.5091 318.7751 0024942 258.6351 101.2046 14.59891382 09
| Epoch (UTC): | 30 May 2026 11:38:41 |
| Eccentricity: | 0.0024942 |
| inclination: | 98.5091° |
| perigee height: | 676 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 318.7751° |
| argument of perigee: | 258.6351° |
| revolutions per day: | 14.59891382 |
| mean anomaly at epoch: | 101.2046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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