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 53871U 26145.10370127 +.00000000 +00000-0 +32263-4 0 00006
2 53871 53.2135 280.7054 0001210 86.5543 273.5587 15.08838684 04
| Epoch (UTC): | 25 May 2026 02:29:19 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 280.7054° |
| argument of perigee: | 86.5543° |
| revolutions per day: | 15.08838684 |
| mean anomaly at epoch: | 273.5587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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