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 61577U 26145.35605053 +.00000000 +00000-0 +91354-5 0 00001
2 61577 53.1588 278.1666 0000602 96.9650 263.1437 15.69714182 07
| Epoch (UTC): | 25 May 2026 08:32:42 |
| Eccentricity: | 0.0000602 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 278.1666° |
| argument of perigee: | 96.9650° |
| revolutions per day: | 15.69714182 |
| mean anomaly at epoch: | 263.1437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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