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 26038.99606272 +.00000000 +00000-0 +69614-4 0 00008
2 24298 70.7565 238.0900 0017583 189.5775 170.5012 14.12407097 06
| Epoch (UTC): | 07 February 2026 23:54:19 |
| Eccentricity: | 0.0017583 |
| inclination: | 70.7565° |
| perigee height: | 838 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 238.0900° |
| argument of perigee: | 189.5775° |
| revolutions per day: | 14.12407097 |
| mean anomaly at epoch: | 170.5012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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