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 61778U 26145.59204999 +.00000000 +00000-0 +62973-3 0 00007
2 61778 97.2936 20.8332 0007342 29.2280 330.9384 15.55686174 02
| Epoch (UTC): | 25 May 2026 14:12:33 |
| Eccentricity: | 0.0007342 |
| inclination: | 97.2936° |
| perigee height: | 395 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 20.8332° |
| argument of perigee: | 29.2280° |
| revolutions per day: | 15.55686174 |
| mean anomaly at epoch: | 330.9384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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