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 01458U 26034.53841931 +.00000000 +00000-0 +00000-0 0 00000
2 01458 27.3672 17.4526 5057032 313.1022 357.7419 0.21365054 08
| Epoch (UTC): | 03 February 2026 12:55:19 |
| Eccentricity: | 0.5057032 |
| inclination: | 27.3672° |
| perigee height: | 52045 km |
| apogee height: | 171589 km |
| right ascension of ascending node: | 17.4526° |
| argument of perigee: | 313.1022° |
| revolutions per day: | 0.21365054 |
| mean anomaly at epoch: | 357.7419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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