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 60037U 26145.54615706 +.00000000 +00000-0 -88773-5 0 00000
2 60037 53.1609 78.4127 0001238 84.4818 275.6324 15.30187491 06
| Epoch (UTC): | 25 May 2026 13:06:27 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.4127° |
| argument of perigee: | 84.4818° |
| revolutions per day: | 15.30187491 |
| mean anomaly at epoch: | 275.6324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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