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 60734U 26145.55365051 +.00000000 +00000-0 +57841-4 0 00000
2 60734 53.1604 271.7897 0001168 82.6594 277.4539 15.30197888 09
| Epoch (UTC): | 25 May 2026 13:17:15 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 271.7897° |
| argument of perigee: | 82.6594° |
| revolutions per day: | 15.30197888 |
| mean anomaly at epoch: | 277.4539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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