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 60143U 26145.52104760 +.00000000 +00000-0 -54098-4 0 00001
2 60143 53.1616 322.7104 0000937 96.0769 264.0339 15.30185207 02
| Epoch (UTC): | 25 May 2026 12:30:18 |
| Eccentricity: | 0.0000937 |
| inclination: | 53.1616° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 322.7104° |
| argument of perigee: | 96.0769° |
| revolutions per day: | 15.30185207 |
| mean anomaly at epoch: | 264.0339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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