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 60273U 26145.48880422 +.00000000 +00000-0 +60973-5 0 00005
2 60273 53.1612 55.9464 0001311 83.1330 276.9820 15.30189539 03
| Epoch (UTC): | 25 May 2026 11:43:52 |
| Eccentricity: | 0.0001311 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.9464° |
| argument of perigee: | 83.1330° |
| revolutions per day: | 15.30189539 |
| mean anomaly at epoch: | 276.9820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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