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 43815U 26145.60240325 +.00000000 +00000-0 +12715-3 0 00003
2 43815 97.3805 221.8526 0016065 28.5857 107.4382 15.27132202 04
| Epoch (UTC): | 25 May 2026 14:27:27 |
| Eccentricity: | 0.0016065 |
| inclination: | 97.3805° |
| perigee height: | 473 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 221.8526° |
| argument of perigee: | 28.5857° |
| revolutions per day: | 15.27132202 |
| mean anomaly at epoch: | 107.4382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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