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 61247U 26144.99363420 +.00000000 +00000-0 +12046-4 0 00003
2 61247 53.1594 39.9128 0001119 72.7567 287.3573 15.69693500 06
| Epoch (UTC): | 24 May 2026 23:50:49 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 39.9128° |
| argument of perigee: | 72.7567° |
| revolutions per day: | 15.69693500 |
| mean anomaly at epoch: | 287.3573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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