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 61517U 26145.41375970 +.00000000 +00000-0 -16406-4 0 00009
2 61517 53.1589 146.4164 0001109 80.6829 279.4298 15.30188537 05
| Epoch (UTC): | 25 May 2026 09:55:48 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.4164° |
| argument of perigee: | 80.6829° |
| revolutions per day: | 15.30188537 |
| mean anomaly at epoch: | 279.4298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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