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 60334U 26145.50935037 +.00000000 +00000-0 +19078-4 0 00008
2 60334 53.1607 79.0136 0001169 86.9455 273.1680 15.30195382 04
| Epoch (UTC): | 25 May 2026 12:13:27 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 79.0136° |
| argument of perigee: | 86.9455° |
| revolutions per day: | 15.30195382 |
| mean anomaly at epoch: | 273.1680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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