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 67215U 26145.54511604 +.00000000 +00000-0 -12872-3 0 00002
2 67215 70.0017 340.8043 0002761 269.9438 90.1404 14.98324757 05
| Epoch (UTC): | 25 May 2026 13:04:58 |
| Eccentricity: | 0.0002761 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.8043° |
| argument of perigee: | 269.9438° |
| revolutions per day: | 14.98324757 |
| mean anomaly at epoch: | 90.1404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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