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 26049.83176617 +.00000000 +00000-0 +68999-4 0 00003
2 24298 70.7574 215.1526 0016798 175.0270 185.1019 14.12410279 08
| Epoch (UTC): | 18 February 2026 19:57:44 |
| Eccentricity: | 0.0016798 |
| inclination: | 70.7574° |
| perigee height: | 839 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 215.1526° |
| argument of perigee: | 175.0270° |
| revolutions per day: | 14.12410279 |
| mean anomaly at epoch: | 185.1019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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