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 61952U 26145.26407589 +.00000000 +00000-0 +32035-3 0 00001
2 61952 53.1605 146.5199 0000733 97.7124 262.3960 15.30201455 07
| Epoch (UTC): | 25 May 2026 06:20:16 |
| Eccentricity: | 0.0000733 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.5199° |
| argument of perigee: | 97.7124° |
| revolutions per day: | 15.30201455 |
| mean anomaly at epoch: | 262.3960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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