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 67723U 26145.56441873 +.00000000 +00000-0 +51800-3 0 00001
2 67723 97.2852 199.0271 0000924 192.2584 167.8636 15.33443267 00
| Epoch (UTC): | 25 May 2026 13:32:45 |
| Eccentricity: | 0.0000924 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.0271° |
| argument of perigee: | 192.2584° |
| revolutions per day: | 15.33443267 |
| mean anomaly at epoch: | 167.8636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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