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 60721U 26145.17000344 +.00000000 +00000-0 +87825-5 0 00001
2 60721 53.1588 99.4967 0001019 68.2603 291.8523 15.69707489 04
| Epoch (UTC): | 25 May 2026 04:04:48 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 99.4967° |
| argument of perigee: | 68.2603° |
| revolutions per day: | 15.69707489 |
| mean anomaly at epoch: | 291.8523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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