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 61691U 26144.90795639 +.00000000 +00000-0 +79116-5 0 00000
2 61691 53.1583 10.5973 0000717 62.3916 297.7174 15.69700956 02
| Epoch (UTC): | 24 May 2026 21:47:27 |
| Eccentricity: | 0.0000717 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 10.5973° |
| argument of perigee: | 62.3916° |
| revolutions per day: | 15.69700956 |
| mean anomaly at epoch: | 297.7174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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