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 48786U 26145.36022258 +.00000000 +00000-0 -19815-3 0 00000
2 48786 87.8999 263.7340 0001906 96.5026 263.6321 13.15547711 02
| Epoch (UTC): | 25 May 2026 08:38:43 |
| Eccentricity: | 0.0001906 |
| inclination: | 87.8999° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7340° |
| argument of perigee: | 96.5026° |
| revolutions per day: | 13.15547711 |
| mean anomaly at epoch: | 263.6321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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