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 24948U 26088.09067617 +.00000000 +00000-0 +12984-3 0 00007
2 24948 86.4007 21.6251 0001788 97.3131 262.8270 14.37654105 02
| Epoch (UTC): | 29 March 2026 02:10:34 |
| Eccentricity: | 0.0001788 |
| inclination: | 86.4007° |
| perigee height: | 765 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 21.6251° |
| argument of perigee: | 97.3131° |
| revolutions per day: | 14.37654105 |
| mean anomaly at epoch: | 262.8270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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