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 24292U 26049.34855992 +.00000000 +00000-0 -38820-4 0 00004
2 24292 62.6720 208.1423 5588202 267.6833 30.8506 4.14733486 01
| Epoch (UTC): | 18 February 2026 08:21:55 |
| Eccentricity: | 0.5588202 |
| inclination: | 62.6720° |
| perigee height: | 841 km |
| apogee height: | 19130 km |
| right ascension of ascending node: | 208.1423° |
| argument of perigee: | 267.6833° |
| revolutions per day: | 4.14733486 |
| mean anomaly at epoch: | 30.8506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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