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 60069U 26145.45283865 +.00000000 +00000-0 +99117-5 0 00005
2 60069 53.1591 173.0916 0001057 71.0110 289.1023 15.69713651 06
| Epoch (UTC): | 25 May 2026 10:52:05 |
| Eccentricity: | 0.0001057 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 173.0916° |
| argument of perigee: | 71.0110° |
| revolutions per day: | 15.69713651 |
| mean anomaly at epoch: | 289.1023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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