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 60429U 26145.41232514 +.00000000 +00000-0 +15625-4 0 00007
2 60429 53.1610 220.9136 0000783 85.4862 274.6228 15.30188061 07
| Epoch (UTC): | 25 May 2026 09:53:44 |
| Eccentricity: | 0.0000783 |
| inclination: | 53.1610° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.9136° |
| argument of perigee: | 85.4862° |
| revolutions per day: | 15.30188061 |
| mean anomaly at epoch: | 274.6228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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