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 60336U 26145.24175772 +.00000000 +00000-0 +33841-4 0 00007
2 60336 53.1608 80.1875 0001335 86.8719 273.2434 15.30199129 08
| Epoch (UTC): | 25 May 2026 05:48:07 |
| Eccentricity: | 0.0001335 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.1875° |
| argument of perigee: | 86.8719° |
| revolutions per day: | 15.30199129 |
| mean anomaly at epoch: | 273.2434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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