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 47802U 26145.58144279 +.00000000 +00000-0 +34218-4 0 00004
2 47802 53.1613 258.1988 0001212 73.3641 286.7493 15.30189135 08
| Epoch (UTC): | 25 May 2026 13:57:16 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 258.1988° |
| argument of perigee: | 73.3641° |
| revolutions per day: | 15.30189135 |
| mean anomaly at epoch: | 286.7493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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