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 61607U 26145.40288676 +.00000000 +00000-0 +10846-2 0 00003
2 61607 87.8854 40.8004 0000985 81.1983 278.9256 13.10370701 02
| Epoch (UTC): | 25 May 2026 09:40:09 |
| Eccentricity: | 0.0000985 |
| inclination: | 87.8854° |
| perigee height: | 1221 km |
| apogee height: | 1222 km |
| right ascension of ascending node: | 40.8004° |
| argument of perigee: | 81.1983° |
| revolutions per day: | 13.10370701 |
| mean anomaly at epoch: | 278.9256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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