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 61746U 26145.49040742 +.00000000 +00000-0 +43528-3 0 00000
2 61746 97.3033 19.1515 0008604 16.8827 343.2708 15.46645297 09
| Epoch (UTC): | 25 May 2026 11:46:11 |
| Eccentricity: | 0.0008604 |
| inclination: | 97.3033° |
| perigee height: | 421 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 19.1515° |
| argument of perigee: | 16.8827° |
| revolutions per day: | 15.46645297 |
| mean anomaly at epoch: | 343.2708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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