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 67217U 26145.26139589 +.00000000 +00000-0 +30934-3 0 00009
2 67217 70.0022 341.4156 0002583 265.3941 94.6923 14.98346132 02
| Epoch (UTC): | 25 May 2026 06:16:24 |
| Eccentricity: | 0.0002583 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.4156° |
| argument of perigee: | 265.3941° |
| revolutions per day: | 14.98346132 |
| mean anomaly at epoch: | 94.6923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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