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 48780U 26145.58219152 +.00000000 +00000-0 -16361-3 0 00002
2 48780 87.9008 263.6841 0001803 98.8086 261.3249 13.15549855 05
| Epoch (UTC): | 25 May 2026 13:58:21 |
| Eccentricity: | 0.0001803 |
| inclination: | 87.9008° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6841° |
| argument of perigee: | 98.8086° |
| revolutions per day: | 13.15549855 |
| mean anomaly at epoch: | 261.3249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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