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 37781U 26145.25623220 +.00000000 +00000-0 +28308-3 0 00003
2 37781 99.3404 148.4322 0006890 132.0277 228.1460 13.74975946 04
| Epoch (UTC): | 25 May 2026 06:08:58 |
| Eccentricity: | 0.0006890 |
| inclination: | 99.3404° |
| perigee height: | 977 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 148.4322° |
| argument of perigee: | 132.0277° |
| revolutions per day: | 13.74975946 |
| mean anomaly at epoch: | 228.1460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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