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 61066U 26145.10389196 +.00000000 +00000-0 +17684-4 0 00007
2 61066 53.1608 96.4104 0001226 97.8346 262.2794 15.30193674 07
| Epoch (UTC): | 25 May 2026 02:29:36 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 96.4104° |
| argument of perigee: | 97.8346° |
| revolutions per day: | 15.30193674 |
| mean anomaly at epoch: | 262.2794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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