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 24278U 26106.87008483 +.00000000 +00000-0 +18688-4 0 00004
2 24278 98.5316 324.1138 0348834 255.5235 100.6968 13.53271232 05
| Epoch (UTC): | 16 April 2026 20:52:55 |
| Eccentricity: | 0.0348834 |
| inclination: | 98.5316° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 324.1138° |
| argument of perigee: | 255.5235° |
| revolutions per day: | 13.53271232 |
| mean anomaly at epoch: | 100.6968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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