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 61621U 26145.54633323 +.00000000 +00000-0 -20748-4 0 00002
2 61621 43.0047 80.1980 0000898 265.9640 94.1109 15.27566665 02
| Epoch (UTC): | 25 May 2026 13:06:43 |
| Eccentricity: | 0.0000898 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.1980° |
| argument of perigee: | 265.9640° |
| revolutions per day: | 15.27566665 |
| mean anomaly at epoch: | 94.1109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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