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 60444U 26145.38219448 +.00000000 +00000-0 +33852-4 0 00003
2 60444 53.1623 220.0119 0000934 98.3251 261.7857 15.34388615 09
| Epoch (UTC): | 25 May 2026 09:10:21 |
| Eccentricity: | 0.0000934 |
| inclination: | 53.1623° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 220.0119° |
| argument of perigee: | 98.3251° |
| revolutions per day: | 15.34388615 |
| mean anomaly at epoch: | 261.7857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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