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 67101U 26145.53075001 +.00000000 +00000-0 +16999-3 0 00004
2 67101 70.0013 180.8623 0003918 265.4475 94.6237 14.98336098 02
| Epoch (UTC): | 25 May 2026 12:44:16 |
| Eccentricity: | 0.0003918 |
| inclination: | 70.0013° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.8623° |
| argument of perigee: | 265.4475° |
| revolutions per day: | 14.98336098 |
| mean anomaly at epoch: | 94.6237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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