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 61700U 26145.45537370 +.00000000 +00000-0 +32814-4 0 00001
2 61700 53.1591 158.8604 0001026 77.6968 282.4147 15.30197051 04
| Epoch (UTC): | 25 May 2026 10:55:44 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 158.8604° |
| argument of perigee: | 77.6968° |
| revolutions per day: | 15.30197051 |
| mean anomaly at epoch: | 282.4147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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