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 41784U 26145.46120803 +.00000000 +00000-0 +14452-3 0 00008
2 41784 97.8179 146.8917 0027487 278.7208 81.0885 14.68937166 06
| Epoch (UTC): | 25 May 2026 11:04:08 |
| Eccentricity: | 0.0027487 |
| inclination: | 97.8179° |
| perigee height: | 645 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 146.8917° |
| argument of perigee: | 278.7208° |
| revolutions per day: | 14.68937166 |
| mean anomaly at epoch: | 81.0885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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