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 24340U 26087.83213331 +.00000000 +00000-0 +25650-2 0 00003
2 24340 81.5994 5.5639 0832316 324.9271 29.9631 13.15980695 07
| Epoch (UTC): | 28 March 2026 19:58:16 |
| Eccentricity: | 0.0832316 |
| inclination: | 81.5994° |
| perigee height: | 569 km |
| apogee height: | 1831 km |
| right ascension of ascending node: | 5.5639° |
| argument of perigee: | 324.9271° |
| revolutions per day: | 13.15980695 |
| mean anomaly at epoch: | 29.9631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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