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 52757U 26145.39771439 +.00000000 +00000-0 +32552-3 0 00000
2 52757 97.6575 302.7963 0005983 145.8497 214.3139 15.50458106 08
| Epoch (UTC): | 25 May 2026 09:32:42 |
| Eccentricity: | 0.0005983 |
| inclination: | 97.6575° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 302.7963° |
| argument of perigee: | 145.8497° |
| revolutions per day: | 15.50458106 |
| mean anomaly at epoch: | 214.3139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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