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 67214U 26145.55347279 +.00000000 +00000-0 +19726-3 0 00001
2 67214 70.0018 340.8336 0002722 265.0949 94.9899 14.98335206 02
| Epoch (UTC): | 25 May 2026 13:17:00 |
| Eccentricity: | 0.0002722 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.8336° |
| argument of perigee: | 265.0949° |
| revolutions per day: | 14.98335206 |
| mean anomaly at epoch: | 94.9899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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