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 24883U 26150.45571338 +.00000000 +00000-0 +12443-3 0 00005
2 24883 98.8672 316.9850 0002529 153.6074 206.5240 14.35543119 08
| Epoch (UTC): | 30 May 2026 10:56:13 |
| Eccentricity: | 0.0002529 |
| inclination: | 98.8672° |
| perigee height: | 771 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 316.9850° |
| argument of perigee: | 153.6074° |
| revolutions per day: | 14.35543119 |
| mean anomaly at epoch: | 206.5240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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