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 60044U 26145.55443552 +.00000000 +00000-0 -72729-5 0 00001
2 60044 53.1592 247.3391 0001159 103.5470 256.5677 15.69701035 01
| Epoch (UTC): | 25 May 2026 13:18:23 |
| Eccentricity: | 0.0001159 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 247.3391° |
| argument of perigee: | 103.5470° |
| revolutions per day: | 15.69701035 |
| mean anomaly at epoch: | 256.5677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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