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 58970U 26145.41304277 +.00000000 +00000-0 +20909-3 0 00001
2 58970 53.1621 300.0663 0001025 74.9954 285.1160 15.30210252 07
| Epoch (UTC): | 25 May 2026 09:54:46 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.0663° |
| argument of perigee: | 74.9954° |
| revolutions per day: | 15.30210252 |
| mean anomaly at epoch: | 285.1160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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