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 67749U 26145.31327706 +.00000000 +00000-0 +34740-3 0 00004
2 67749 97.5029 273.7363 0008774 307.2519 52.7914 15.19468826 09
| Epoch (UTC): | 25 May 2026 07:31:07 |
| Eccentricity: | 0.0008774 |
| inclination: | 97.5029° |
| perigee height: | 501 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 273.7363° |
| argument of perigee: | 307.2519° |
| revolutions per day: | 15.19468826 |
| mean anomaly at epoch: | 52.7914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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