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 48774U 26145.55194538 +.00000000 +00000-0 +44330-3 0 00008
2 48774 87.8992 263.7294 0001846 83.8941 276.2399 13.15547044 02
| Epoch (UTC): | 25 May 2026 13:14:48 |
| Eccentricity: | 0.0001846 |
| inclination: | 87.8992° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7294° |
| argument of perigee: | 83.8941° |
| revolutions per day: | 13.15547044 |
| mean anomaly at epoch: | 276.2399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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