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 61616U 26145.58099972 +.00000000 +00000-0 +17955-3 0 00000
2 61616 97.5221 166.5413 0002939 75.8964 284.2587 15.01023362 05
| Epoch (UTC): | 25 May 2026 13:56:38 |
| Eccentricity: | 0.0002939 |
| inclination: | 97.5221° |
| perigee height: | 562 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 166.5413° |
| argument of perigee: | 75.8964° |
| revolutions per day: | 15.01023362 |
| mean anomaly at epoch: | 284.2587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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