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 45677U 26145.20585418 +.00000000 +00000-0 +12739-2 0 00007
2 45677 53.1529 67.8967 0003352 101.0208 259.1173 15.36819248 09
| Epoch (UTC): | 25 May 2026 04:56:25 |
| Eccentricity: | 0.0003352 |
| inclination: | 53.1529° |
| perigee height: | 453 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 67.8967° |
| argument of perigee: | 101.0208° |
| revolutions per day: | 15.36819248 |
| mean anomaly at epoch: | 259.1173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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