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 57614U 26144.96818860 +.00000000 +00000-0 +31527-4 0 00001
2 57614 43.0035 10.6681 0001449 259.9356 100.1332 15.27571057 09
| Epoch (UTC): | 24 May 2026 23:14:11 |
| Eccentricity: | 0.0001449 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.6681° |
| argument of perigee: | 259.9356° |
| revolutions per day: | 15.27571057 |
| mean anomaly at epoch: | 100.1332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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