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 60057U 26145.11382307 +.00000000 +00000-0 +73462-4 0 00000
2 60057 53.1599 83.2852 0001188 87.3696 272.7441 15.30189586 00
| Epoch (UTC): | 25 May 2026 02:43:54 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 83.2852° |
| argument of perigee: | 87.3696° |
| revolutions per day: | 15.30189586 |
| mean anomaly at epoch: | 272.7441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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