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 17624U 26101.11197550 +.00000000 +00000-0 +89648-3 0 00000
2 17624 82.8393 132.5319 0012068 44.5638 10.6629 14.48507265 02
| Epoch (UTC): | 11 April 2026 02:41:14 |
| Eccentricity: | 0.0012068 |
| inclination: | 82.8393° |
| perigee height: | 722 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 132.5319° |
| argument of perigee: | 44.5638° |
| revolutions per day: | 14.48507265 |
| mean anomaly at epoch: | 10.6629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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