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 24720U 26107.89303675 +.00000000 +00000-0 +13472-2 0 00004
2 24720 31.3160 312.7440 5981001 164.8324 351.1842 3.84772731 00
| Epoch (UTC): | 17 April 2026 21:25:58 |
| Eccentricity: | 0.5981001 |
| inclination: | 31.3160° |
| perigee height: | 536 km |
| apogee height: | 21114 km |
| right ascension of ascending node: | 312.7440° |
| argument of perigee: | 164.8324° |
| revolutions per day: | 3.84772731 |
| mean anomaly at epoch: | 351.1842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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