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 61735U 26145.61913318 +.00000000 +00000-0 +33198-4 0 00003
2 61735 98.7203 19.0265 0001089 139.6582 220.4676 14.22749563 08
| Epoch (UTC): | 25 May 2026 14:51:33 |
| Eccentricity: | 0.0001089 |
| inclination: | 98.7203° |
| perigee height: | 815 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 19.0265° |
| argument of perigee: | 139.6582° |
| revolutions per day: | 14.22749563 |
| mean anomaly at epoch: | 220.4676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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