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 68352U 26145.37618741 +.00000000 +00000-0 +25658-4 0 00002
2 68352 54.9797 129.0816 0010420 79.1040 281.1130 14.73368265 03
| Epoch (UTC): | 25 May 2026 09:01:42 |
| Eccentricity: | 0.0010420 |
| inclination: | 54.9797° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 129.0816° |
| argument of perigee: | 79.1040° |
| revolutions per day: | 14.73368265 |
| mean anomaly at epoch: | 281.1130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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