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 60144U 26145.46839617 +.00000000 +00000-0 +57379-5 0 00006
2 60144 53.1612 323.1367 0001192 91.1765 268.9372 15.30196936 02
| Epoch (UTC): | 25 May 2026 11:14:29 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.1367° |
| argument of perigee: | 91.1765° |
| revolutions per day: | 15.30196936 |
| mean anomaly at epoch: | 268.9372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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