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 60014U 26145.60147906 +.00000000 +00000-0 +92341-4 0 00008
2 60014 97.5446 221.6126 0011050 219.5266 140.5152 14.98170773 01
| Epoch (UTC): | 25 May 2026 14:26:07 |
| Eccentricity: | 0.0011050 |
| inclination: | 97.5446° |
| perigee height: | 565 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 221.6126° |
| argument of perigee: | 219.5266° |
| revolutions per day: | 14.98170773 |
| mean anomaly at epoch: | 140.5152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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