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 52151U 26145.60727572 +.00000000 +00000-0 +11141-3 0 00002
2 52151 97.8623 331.1274 0010122 280.0700 79.9378 14.94291119 09
| Epoch (UTC): | 25 May 2026 14:34:28 |
| Eccentricity: | 0.0010122 |
| inclination: | 97.8623° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 331.1274° |
| argument of perigee: | 280.0700° |
| revolutions per day: | 14.94291119 |
| mean anomaly at epoch: | 79.9378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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