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 61239U 26145.59220497 +.00000000 +00000-0 +17875-3 0 00001
2 61239 97.4483 149.6395 0021372 12.2402 347.9342 15.10025546 02
| Epoch (UTC): | 25 May 2026 14:12:46 |
| Eccentricity: | 0.0021372 |
| inclination: | 97.4483° |
| perigee height: | 521 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 149.6395° |
| argument of perigee: | 12.2402° |
| revolutions per day: | 15.10025546 |
| mean anomaly at epoch: | 347.9342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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