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 67102U 26145.24840272 +.00000000 +00000-0 +70887-3 0 00009
2 67102 42.9987 96.7434 0000579 266.3794 93.6992 15.27605841 05
| Epoch (UTC): | 25 May 2026 05:57:41 |
| Eccentricity: | 0.0000579 |
| inclination: | 42.9987° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 96.7434° |
| argument of perigee: | 266.3794° |
| revolutions per day: | 15.27605841 |
| mean anomaly at epoch: | 93.6992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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