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 60256U 26145.16538937 +.00000000 +00000-0 +61503-4 0 00001
2 60256 53.1602 57.4858 0001209 84.1776 275.9363 15.30196284 04
| Epoch (UTC): | 25 May 2026 03:58:09 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.4858° |
| argument of perigee: | 84.1776° |
| revolutions per day: | 15.30196284 |
| mean anomaly at epoch: | 275.9363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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