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 67974U 26145.45074066 +.00000000 +00000-0 +87275-3 0 00008
2 67974 97.2858 155.4845 0000611 52.8947 307.2352 15.33462862 01
| Epoch (UTC): | 25 May 2026 10:49:03 |
| Eccentricity: | 0.0000611 |
| inclination: | 97.2858° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4845° |
| argument of perigee: | 52.8947° |
| revolutions per day: | 15.33462862 |
| mean anomaly at epoch: | 307.2352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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