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 24797U 26075.79693546 +.00000000 +00000-0 +15048-3 0 00002
2 24797 86.8876 261.5208 0216865 89.8137 283.2565 14.47839766 08
| Epoch (UTC): | 16 March 2026 19:07:35 |
| Eccentricity: | 0.0216865 |
| inclination: | 86.8876° |
| perigee height: | 579 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 261.5208° |
| argument of perigee: | 89.8137° |
| revolutions per day: | 14.47839766 |
| mean anomaly at epoch: | 283.2565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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