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 37868U 26143.56401742 +.00000000 +00000-0 +00000-0 0 00000
2 37868 65.2635 73.7813 0020438 242.6206 292.2679 2.13102783 03
| Epoch (UTC): | 23 May 2026 13:32:11 |
| Eccentricity: | 0.0020438 |
| inclination: | 65.2635° |
| perigee height: | 19078 km |
| apogee height: | 19182 km |
| right ascension of ascending node: | 73.7813° |
| argument of perigee: | 242.6206° |
| revolutions per day: | 2.13102783 |
| mean anomaly at epoch: | 292.2679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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