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 12708U 26108.91128666 +.00000000 +00000-0 +18529-2 0 00004
2 12708 82.8581 94.1712 0020528 17.0860 343.1035 14.71594715 08
| Epoch (UTC): | 18 April 2026 21:52:15 |
| Eccentricity: | 0.0020528 |
| inclination: | 82.8581° |
| perigee height: | 642 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 94.1712° |
| argument of perigee: | 17.0860° |
| revolutions per day: | 14.71594715 |
| mean anomaly at epoch: | 343.1035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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