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 67980U 26145.49966102 +.00000000 +00000-0 -21989-3 0 00001
2 67980 97.2831 155.5685 0000695 65.9950 294.1365 15.33458427 03
| Epoch (UTC): | 25 May 2026 11:59:30 |
| Eccentricity: | 0.0000695 |
| inclination: | 97.2831° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5685° |
| argument of perigee: | 65.9950° |
| revolutions per day: | 15.33458427 |
| mean anomaly at epoch: | 294.1365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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