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 61662U 26145.26835242 +.00000000 +00000-0 +11595-4 0 00009
2 61662 53.1614 95.1333 0001300 87.6339 272.4811 15.31704155 04
| Epoch (UTC): | 25 May 2026 06:26:25 |
| Eccentricity: | 0.0001300 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.1333° |
| argument of perigee: | 87.6339° |
| revolutions per day: | 15.31704155 |
| mean anomaly at epoch: | 272.4811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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