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 60067U 26145.33531000 +.00000000 +00000-0 -47103-4 0 00005
2 60067 53.1596 173.7874 0001025 59.7207 300.3913 15.69732102 00
| Epoch (UTC): | 25 May 2026 08:02:50 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 173.7874° |
| argument of perigee: | 59.7207° |
| revolutions per day: | 15.69732102 |
| mean anomaly at epoch: | 300.3913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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