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 61927U 26145.56504626 +.00000000 +00000-0 +69992-3 0 00008
2 61927 43.0016 207.2097 0002933 268.2766 91.7749 15.27597414 04
| Epoch (UTC): | 25 May 2026 13:33:39 |
| Eccentricity: | 0.0002933 |
| inclination: | 43.0016° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 207.2097° |
| argument of perigee: | 268.2766° |
| revolutions per day: | 15.27597414 |
| mean anomaly at epoch: | 91.7749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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