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 47837U 26145.54298594 +.00000000 +00000-0 +22416-3 0 00004
2 47837 53.1587 241.5713 0001284 66.3448 293.7688 15.31702880 07
| Epoch (UTC): | 25 May 2026 13:01:53 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 241.5713° |
| argument of perigee: | 66.3448° |
| revolutions per day: | 15.31702880 |
| mean anomaly at epoch: | 293.7688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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