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 39624U 26145.57965235 +.00000000 +00000-0 +92518-4 0 00006
2 39624 97.9493 173.1999 0015202 60.3720 299.8994 14.61827166 06
| Epoch (UTC): | 25 May 2026 13:54:41 |
| Eccentricity: | 0.0015202 |
| inclination: | 97.9493° |
| perigee height: | 677 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 173.1999° |
| argument of perigee: | 60.3720° |
| revolutions per day: | 14.61827166 |
| mean anomaly at epoch: | 299.8994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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