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 67099U 26145.41808830 +.00000000 +00000-0 +34849-3 0 00005
2 67099 70.0016 180.8836 0003686 268.7680 91.3057 14.98324254 08
| Epoch (UTC): | 25 May 2026 10:02:02 |
| Eccentricity: | 0.0003686 |
| inclination: | 70.0016° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.8836° |
| argument of perigee: | 268.7680° |
| revolutions per day: | 14.98324254 |
| mean anomaly at epoch: | 91.3057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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