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 24298U 26041.47482073 +.00000000 +00000-0 +78326-4 0 00006
2 24298 70.7565 232.8428 0017402 186.3162 173.7741 14.12407804 08
| Epoch (UTC): | 10 February 2026 11:23:44 |
| Eccentricity: | 0.0017402 |
| inclination: | 70.7565° |
| perigee height: | 839 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 232.8428° |
| argument of perigee: | 186.3162° |
| revolutions per day: | 14.12407804 |
| mean anomaly at epoch: | 173.7741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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