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 39630U 26146.23718242 +.00000000 +00000-0 +99109-4 0 00004
2 39630 98.7815 146.4873 0009172 272.0683 87.9441 14.14971384 06
| Epoch (UTC): | 26 May 2026 05:41:32 |
| Eccentricity: | 0.0009172 |
| inclination: | 98.7815° |
| perigee height: | 836 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 146.4873° |
| argument of perigee: | 272.0683° |
| revolutions per day: | 14.14971384 |
| mean anomaly at epoch: | 87.9441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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