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 67098U 26145.49719169 +.00000000 +00000-0 +15345-3 0 00008
2 67098 70.0010 180.7500 0004177 267.3895 92.6786 14.98335023 06
| Epoch (UTC): | 25 May 2026 11:55:57 |
| Eccentricity: | 0.0004177 |
| inclination: | 70.0010° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.7500° |
| argument of perigee: | 267.3895° |
| revolutions per day: | 14.98335023 |
| mean anomaly at epoch: | 92.6786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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