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 26071.60397799 +.00000000 +00000-0 +45667-4 0 00004
2 24278 98.5377 293.6293 0349702 347.2088 12.0349 13.53268870 07
| Epoch (UTC): | 12 March 2026 14:29:43 |
| Eccentricity: | 0.0349702 |
| inclination: | 98.5377° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 293.6293° |
| argument of perigee: | 347.2088° |
| revolutions per day: | 13.53268870 |
| mean anomaly at epoch: | 12.0349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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