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 67752U 26145.31436208 +.00000000 +00000-0 +29607-3 0 00002
2 67752 97.5033 272.9825 0011466 334.6596 25.4071 15.13109700 01
| Epoch (UTC): | 25 May 2026 07:32:40 |
| Eccentricity: | 0.0011466 |
| inclination: | 97.5033° |
| perigee height: | 519 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 272.9825° |
| argument of perigee: | 334.6596° |
| revolutions per day: | 15.13109700 |
| mean anomaly at epoch: | 25.4071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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