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 26135.18771387 +.00000000 +00000-0 +41226-4 0 00004
2 24278 98.5275 348.5741 0349825 181.9145 178.0679 13.53272480 06
| Epoch (UTC): | 15 May 2026 04:30:18 |
| Eccentricity: | 0.0349825 |
| inclination: | 98.5275° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 348.5741° |
| argument of perigee: | 181.9145° |
| revolutions per day: | 13.53272480 |
| mean anomaly at epoch: | 178.0679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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