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 24239U 26088.17157975 +.00000000 +00000-0 +16220-2 0 00002
2 24239 81.5080 244.8365 0142759 103.5321 258.1840 14.80170296 05
| Epoch (UTC): | 29 March 2026 04:07:04 |
| Eccentricity: | 0.0142759 |
| inclination: | 81.5080° |
| perigee height: | 529 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 244.8365° |
| argument of perigee: | 103.5321° |
| revolutions per day: | 14.80170296 |
| mean anomaly at epoch: | 258.1840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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