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 60342U 26145.09741256 +.00000000 +00000-0 +25107-4 0 00009
2 60342 53.1608 80.7072 0001435 90.5243 269.5922 15.30194231 04
| Epoch (UTC): | 25 May 2026 02:20:16 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.7072° |
| argument of perigee: | 90.5243° |
| revolutions per day: | 15.30194231 |
| mean anomaly at epoch: | 269.5922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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