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 60302U 26145.23121421 +.00000000 +00000-0 -77401-5 0 00003
2 60302 53.1589 129.0644 0001215 74.6459 285.4693 15.69697622 04
| Epoch (UTC): | 25 May 2026 05:32:56 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 129.0644° |
| argument of perigee: | 74.6459° |
| revolutions per day: | 15.69697622 |
| mean anomaly at epoch: | 285.4693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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