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 44552U 26144.34448323 +.00000000 +00000-0 +00000-0 0 00001
2 44552 62.7116 159.1737 6488261 272.1353 20.3581 2.00616985 02
| Epoch (UTC): | 24 May 2026 08:16:03 |
| Eccentricity: | 0.6488261 |
| inclination: | 62.7116° |
| perigee height: | 2948 km |
| apogee height: | 37407 km |
| right ascension of ascending node: | 159.1737° |
| argument of perigee: | 272.1353° |
| revolutions per day: | 2.00616985 |
| mean anomaly at epoch: | 20.3581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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