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 60400U 26145.07933096 +.00000000 +00000-0 +14868-4 0 00009
2 60400 53.1570 69.4807 0000774 98.3997 261.7109 15.69710643 08
| Epoch (UTC): | 25 May 2026 01:54:14 |
| Eccentricity: | 0.0000774 |
| inclination: | 53.1570° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 69.4807° |
| argument of perigee: | 98.3997° |
| revolutions per day: | 15.69710643 |
| mean anomaly at epoch: | 261.7109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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