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 61707U 26145.18909219 +.00000000 +00000-0 +16370-4 0 00002
2 61707 53.1603 105.6817 0001260 96.3539 263.7605 15.30191506 03
| Epoch (UTC): | 25 May 2026 04:32:17 |
| Eccentricity: | 0.0001260 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.6817° |
| argument of perigee: | 96.3539° |
| revolutions per day: | 15.30191506 |
| mean anomaly at epoch: | 263.7605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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