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 26140.58018858 +.00000000 +00000-0 +60072-4 0 00009
2 39630 98.7816 140.9187 0009234 290.2692 69.7489 14.14969373 00
| Epoch (UTC): | 20 May 2026 13:55:28 |
| Eccentricity: | 0.0009234 |
| inclination: | 98.7816° |
| perigee height: | 836 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 140.9187° |
| argument of perigee: | 290.2692° |
| revolutions per day: | 14.14969373 |
| mean anomaly at epoch: | 69.7489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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