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 61681U 26145.24715544 +.00000000 +00000-0 +24574-4 0 00001
2 61681 53.1608 95.7045 0001732 105.0486 255.0707 15.30190379 08
| Epoch (UTC): | 25 May 2026 05:55:54 |
| Eccentricity: | 0.0001732 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.7045° |
| argument of perigee: | 105.0486° |
| revolutions per day: | 15.30190379 |
| mean anomaly at epoch: | 255.0707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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