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 61565U 26145.61313045 +.00000000 +00000-0 +11001-3 0 00003
2 61565 88.9873 64.1321 0008549 323.4475 36.6092 13.50784048 05
| Epoch (UTC): | 25 May 2026 14:42:54 |
| Eccentricity: | 0.0008549 |
| inclination: | 88.9873° |
| perigee height: | 1063 km |
| apogee height: | 1076 km |
| right ascension of ascending node: | 64.1321° |
| argument of perigee: | 323.4475° |
| revolutions per day: | 13.50784048 |
| mean anomaly at epoch: | 36.6092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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