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 61245U 26145.12587265 +.00000000 +00000-0 +80015-5 0 00004
2 61245 53.1585 39.3236 0000875 76.8203 283.2913 15.69704535 02
| Epoch (UTC): | 25 May 2026 03:01:15 |
| Eccentricity: | 0.0000875 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 39.3236° |
| argument of perigee: | 76.8203° |
| revolutions per day: | 15.69704535 |
| mean anomaly at epoch: | 283.2913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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