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 61690U 26145.04510353 +.00000000 +00000-0 +38980-4 0 00006
2 61690 53.1575 10.0355 0000913 50.8755 309.2344 15.69716188 04
| Epoch (UTC): | 25 May 2026 01:04:56 |
| Eccentricity: | 0.0000913 |
| inclination: | 53.1575° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 10.0355° |
| argument of perigee: | 50.8755° |
| revolutions per day: | 15.69716188 |
| mean anomaly at epoch: | 309.2344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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