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 61771U 26145.60411620 +.00000000 +00000-0 +59835-3 0 00006
2 61771 97.2969 20.9924 0008000 30.1630 330.0084 15.55841079 06
| Epoch (UTC): | 25 May 2026 14:29:55 |
| Eccentricity: | 0.0008000 |
| inclination: | 97.2969° |
| perigee height: | 394 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 20.9924° |
| argument of perigee: | 30.1630° |
| revolutions per day: | 15.55841079 |
| mean anomaly at epoch: | 330.0084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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