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 26040.48331764 +.00000000 +00000-0 +75946-4 0 00001
2 24298 70.7565 234.9417 0017477 187.6237 172.4620 14.12407540 07
| Epoch (UTC): | 09 February 2026 11:35:58 |
| Eccentricity: | 0.0017477 |
| inclination: | 70.7565° |
| perigee height: | 839 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 234.9417° |
| argument of perigee: | 187.6237° |
| revolutions per day: | 14.12407540 |
| mean anomaly at epoch: | 172.4620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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