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 67969U 26145.45889896 +.00000000 +00000-0 +42552-3 0 00006
2 67969 97.2841 155.4734 0001329 95.1585 264.9809 15.33454516 02
| Epoch (UTC): | 25 May 2026 11:00:48 |
| Eccentricity: | 0.0001329 |
| inclination: | 97.2841° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4734° |
| argument of perigee: | 95.1585° |
| revolutions per day: | 15.33454516 |
| mean anomaly at epoch: | 264.9809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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