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 43275U 26145.61725215 +.00000000 +00000-0 -18546-3 0 00009
2 43275 63.3928 149.3551 0273437 7.3272 353.1625 13.45458409 07
| Epoch (UTC): | 25 May 2026 14:48:50 |
| Eccentricity: | 0.0273437 |
| inclination: | 63.3928° |
| perigee height: | 885 km |
| apogee height: | 1293 km |
| right ascension of ascending node: | 149.3551° |
| argument of perigee: | 7.3272° |
| revolutions per day: | 13.45458409 |
| mean anomaly at epoch: | 353.1625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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