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 26073.30413812 +.00000000 +00000-0 +76934-3 0 00005
2 40024 98.0842 97.4678 0005007 137.2432 222.9196 15.28315368 01
| Epoch (UTC): | 14 March 2026 07:17:57 |
| Eccentricity: | 0.0005007 |
| inclination: | 98.0842° |
| perigee height: | 477 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 97.4678° |
| argument of perigee: | 137.2432° |
| revolutions per day: | 15.28315368 |
| mean anomaly at epoch: | 222.9196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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