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 67621U 26145.47897807 +.00000000 +00000-0 +98000-3 0 00003
2 67621 43.0039 66.4358 0000412 283.4608 76.6197 15.27582703 09
| Epoch (UTC): | 25 May 2026 11:29:43 |
| Eccentricity: | 0.0000412 |
| inclination: | 43.0039° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 66.4358° |
| argument of perigee: | 283.4608° |
| revolutions per day: | 15.27582703 |
| mean anomaly at epoch: | 76.6197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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