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 48787U 26145.56305198 +.00000000 +00000-0 +21470-3 0 00009
2 48787 87.9002 263.6909 0001827 72.3523 287.7807 13.15549567 02
| Epoch (UTC): | 25 May 2026 13:30:47 |
| Eccentricity: | 0.0001827 |
| inclination: | 87.9002° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6909° |
| argument of perigee: | 72.3523° |
| revolutions per day: | 13.15549567 |
| mean anomaly at epoch: | 287.7807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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