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 52471U 26145.49341038 +.00000000 +00000-0 +29022-4 0 00001
2 52471 53.2135 74.3433 0001384 87.1375 272.9776 15.08832188 05
| Epoch (UTC): | 25 May 2026 11:50:30 |
| Eccentricity: | 0.0001384 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.3433° |
| argument of perigee: | 87.1375° |
| revolutions per day: | 15.08832188 |
| mean anomaly at epoch: | 272.9776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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