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 60329U 26145.23201514 +.00000000 +00000-0 +47691-4 0 00000
2 60329 53.1604 80.1294 0001273 76.8425 283.2718 15.31706970 00
| Epoch (UTC): | 25 May 2026 05:34:06 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 80.1294° |
| argument of perigee: | 76.8425° |
| revolutions per day: | 15.31706970 |
| mean anomaly at epoch: | 283.2718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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