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 37739U 26145.18982882 +.00000000 +00000-0 +36860-4 0 00003
2 37739 51.9857 82.5544 0000556 22.0570 116.6147 12.62262568 02
| Epoch (UTC): | 25 May 2026 04:33:21 |
| Eccentricity: | 0.0000556 |
| inclination: | 51.9857° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 82.5544° |
| argument of perigee: | 22.0570° |
| revolutions per day: | 12.62262568 |
| mean anomaly at epoch: | 116.6147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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