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 38736U 26088.15865457 +.00000000 +00000-0 +38411-4 0 00006
2 38736 82.4765 120.8252 0024233 225.5974 134.3122 12.43901330 01
| Epoch (UTC): | 29 March 2026 03:48:27 |
| Eccentricity: | 0.0024233 |
| inclination: | 82.4765° |
| perigee height: | 1471 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 120.8252° |
| argument of perigee: | 225.5974° |
| revolutions per day: | 12.43901330 |
| mean anomaly at epoch: | 134.3122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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