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 65413U 26145.59151601 +.00000000 +00000-0 +45163-3 0 00000
2 65413 53.1584 235.4719 0001113 85.9302 274.1826 15.30201363 05
| Epoch (UTC): | 25 May 2026 14:11:46 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.4719° |
| argument of perigee: | 85.9302° |
| revolutions per day: | 15.30201363 |
| mean anomaly at epoch: | 274.1826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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