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 26046.17132251 +.00000000 +00000-0 +56200-4 0 00003
2 24278 98.5413 271.6334 0350679 53.1218 310.1529 13.53267064 09
| Epoch (UTC): | 15 February 2026 04:06:42 |
| Eccentricity: | 0.0350679 |
| inclination: | 98.5413° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 271.6334° |
| argument of perigee: | 53.1218° |
| revolutions per day: | 13.53267064 |
| mean anomaly at epoch: | 310.1529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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