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 68629U 26145.41395793 +.00000000 +00000-0 +41390-3 0 00003
2 68629 60.0211 265.5756 0025354 4.3159 355.8136 15.24421624 02
| Epoch (UTC): | 25 May 2026 09:56:05 |
| Eccentricity: | 0.0025354 |
| inclination: | 60.0211° |
| perigee height: | 475 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 265.5756° |
| argument of perigee: | 4.3159° |
| revolutions per day: | 15.24421624 |
| mean anomaly at epoch: | 355.8136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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