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 60396U 26145.54148181 +.00000000 +00000-0 +12250-3 0 00000
2 60396 88.9720 281.9762 0016141 79.0407 281.2559 13.51011124 06
| Epoch (UTC): | 25 May 2026 12:59:44 |
| Eccentricity: | 0.0016141 |
| inclination: | 88.9720° |
| perigee height: | 1057 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 281.9762° |
| argument of perigee: | 79.0407° |
| revolutions per day: | 13.51011124 |
| mean anomaly at epoch: | 281.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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