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 40024U 26032.49219181 +.00000000 +00000-0 +53295-3 0 00008
2 40024 98.0867 53.2430 0002343 317.5965 42.5090 15.26670760 05
| Epoch (UTC): | 01 February 2026 11:48:45 |
| Eccentricity: | 0.0002343 |
| inclination: | 98.0867° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 53.2430° |
| argument of perigee: | 317.5965° |
| revolutions per day: | 15.26670760 |
| mean anomaly at epoch: | 42.5090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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