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 61762U 26145.50906101 +.00000000 +00000-0 +11331-2 0 00006
2 61762 97.2868 27.8956 0002396 154.1258 206.0135 15.90777534 02
| Epoch (UTC): | 25 May 2026 12:13:02 |
| Eccentricity: | 0.0002396 |
| inclination: | 97.2868° |
| perigee height: | 299 km |
| apogee height: | 302 km |
| right ascension of ascending node: | 27.8956° |
| argument of perigee: | 154.1258° |
| revolutions per day: | 15.90777534 |
| mean anomaly at epoch: | 206.0135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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