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 57972U 26144.73649453 +.00000000 +00000-0 +87200-3 0 00001
2 57972 43.0024 266.7858 0001949 266.7215 93.3414 15.27598536 04
| Epoch (UTC): | 24 May 2026 17:40:33 |
| Eccentricity: | 0.0001949 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.7858° |
| argument of perigee: | 266.7215° |
| revolutions per day: | 15.27598536 |
| mean anomaly at epoch: | 93.3414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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