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 26046.92808350 +.00000000 +00000-0 +86294-4 0 00004
2 24298 70.7569 221.2989 0016980 178.9391 181.1767 14.12409561 00
| Epoch (UTC): | 15 February 2026 22:16:26 |
| Eccentricity: | 0.0016980 |
| inclination: | 70.7569° |
| perigee height: | 839 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 221.2989° |
| argument of perigee: | 178.9391° |
| revolutions per day: | 14.12409561 |
| mean anomaly at epoch: | 181.1767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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