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 24925U 26088.18060817 +.00000000 +00000-0 +55037-4 0 00004
2 24925 86.3399 3.4477 0005526 195.2145 164.8915 14.87295541 02
| Epoch (UTC): | 29 March 2026 04:20:04 |
| Eccentricity: | 0.0005526 |
| inclination: | 86.3399° |
| perigee height: | 603 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 3.4477° |
| argument of perigee: | 195.2145° |
| revolutions per day: | 14.87295541 |
| mean anomaly at epoch: | 164.8915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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