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 10521U 26159.17134330 +.00000000 +00000-0 +96796-4 0 00008
2 10521 74.0269 315.5603 0021128 250.2523 109.6355 14.42442250 02
| Epoch (UTC): | 08 June 2026 04:06:44 |
| Eccentricity: | 0.0021128 |
| inclination: | 74.0269° |
| perigee height: | 735 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 315.5603° |
| argument of perigee: | 250.2523° |
| revolutions per day: | 14.42442250 |
| mean anomaly at epoch: | 109.6355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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