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 67622U 26145.19818066 +.00000000 +00000-0 +16564-2 0 00007
2 67622 42.9997 67.7855 0001155 269.2443 90.8276 15.27596757 01
| Epoch (UTC): | 25 May 2026 04:45:22 |
| Eccentricity: | 0.0001155 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.7855° |
| argument of perigee: | 269.2443° |
| revolutions per day: | 15.27596757 |
| mean anomaly at epoch: | 90.8276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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