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 60520U 26145.15951765 +.00000000 +00000-0 +72921-3 0 00007
2 60520 97.3772 237.2959 0001121 308.7047 51.4111 15.63150510 01
| Epoch (UTC): | 25 May 2026 03:49:42 |
| Eccentricity: | 0.0001121 |
| inclination: | 97.3772° |
| perigee height: | 378 km |
| apogee height: | 379 km |
| right ascension of ascending node: | 237.2959° |
| argument of perigee: | 308.7047° |
| revolutions per day: | 15.63150510 |
| mean anomaly at epoch: | 51.4111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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