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 26045.93658184 +.00000000 +00000-0 +78249-4 0 00003
2 24298 70.7569 223.3977 0017011 180.3154 179.7958 14.12409126 02
| Epoch (UTC): | 14 February 2026 22:28:40 |
| Eccentricity: | 0.0017011 |
| inclination: | 70.7569° |
| perigee height: | 839 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 223.3977° |
| argument of perigee: | 180.3154° |
| revolutions per day: | 14.12409126 |
| mean anomaly at epoch: | 179.7958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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