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 57517U 26143.85198882 +.00000000 +00000-0 +00000-0 0 00003
2 57517 65.2892 73.4407 0011626 296.5431 63.3318 2.13103740 05
| Epoch (UTC): | 23 May 2026 20:26:51 |
| Eccentricity: | 0.0011626 |
| inclination: | 65.2892° |
| perigee height: | 19100 km |
| apogee height: | 19159 km |
| right ascension of ascending node: | 73.4407° |
| argument of perigee: | 296.5431° |
| revolutions per day: | 2.13103740 |
| mean anomaly at epoch: | 63.3318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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