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 24827U 26138.11309589 +.00000000 +00000-0 -95407-3 0 00001
2 24827 63.3053 256.2930 1090453 69.3451 90.6350 11.07977087 02
| Epoch (UTC): | 18 May 2026 02:42:51 |
| Eccentricity: | 0.1090453 |
| inclination: | 63.3053° |
| perigee height: | 1194 km |
| apogee height: | 3048 km |
| right ascension of ascending node: | 256.2930° |
| argument of perigee: | 69.3451° |
| revolutions per day: | 11.07977087 |
| mean anomaly at epoch: | 90.6350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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