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 60146U 26145.51893593 +.00000000 +00000-0 +20656-4 0 00004
2 60146 53.1614 322.7369 0001109 92.5748 267.5380 15.30196610 00
| Epoch (UTC): | 25 May 2026 12:27:16 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 322.7369° |
| argument of perigee: | 92.5748° |
| revolutions per day: | 15.30196610 |
| mean anomaly at epoch: | 267.5380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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