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 60363U 26145.49271064 +.00000000 +00000-0 +62439-4 0 00000
2 60363 53.1614 313.0628 0000983 91.2947 268.8166 15.30200156 05
| Epoch (UTC): | 25 May 2026 11:49:30 |
| Eccentricity: | 0.0000983 |
| inclination: | 53.1614° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0628° |
| argument of perigee: | 91.2947° |
| revolutions per day: | 15.30200156 |
| mean anomaly at epoch: | 268.8166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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