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 44538U 26145.67947365 +.00000000 +00000-0 +53502-3 0 00000
2 44538 97.5362 294.5768 0007425 33.8199 326.3523 15.48311999 04
| Epoch (UTC): | 25 May 2026 16:18:26 |
| Eccentricity: | 0.0007425 |
| inclination: | 97.5362° |
| perigee height: | 417 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 294.5768° |
| argument of perigee: | 33.8199° |
| revolutions per day: | 15.48311999 |
| mean anomaly at epoch: | 326.3523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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