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 67645U 26145.49553986 +.00000000 +00000-0 +93184-3 0 00006
2 67645 43.0023 65.7017 0000641 70.4400 289.6521 15.27585408 02
| Epoch (UTC): | 25 May 2026 11:53:34 |
| Eccentricity: | 0.0000641 |
| inclination: | 43.0023° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 65.7017° |
| argument of perigee: | 70.4400° |
| revolutions per day: | 15.27585408 |
| mean anomaly at epoch: | 289.6521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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