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 61579U 26145.34624183 +.00000000 +00000-0 +12731-4 0 00008
2 61579 53.1576 278.0995 0000436 58.0641 302.0419 15.69711887 06
| Epoch (UTC): | 25 May 2026 08:18:35 |
| Eccentricity: | 0.0000436 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 278.0995° |
| argument of perigee: | 58.0641° |
| revolutions per day: | 15.69711887 |
| mean anomaly at epoch: | 302.0419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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