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 60070U 26145.38427003 +.00000000 +00000-0 +18635-4 0 00008
2 60070 53.1595 173.3757 0001043 91.2352 268.8786 15.69704650 04
| Epoch (UTC): | 25 May 2026 09:13:20 |
| Eccentricity: | 0.0001043 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 173.3757° |
| argument of perigee: | 91.2352° |
| revolutions per day: | 15.69704650 |
| mean anomaly at epoch: | 268.8786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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