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 53084U 26145.44408041 +.00000000 +00000-0 +10071-3 0 00008
2 53084 97.4478 326.4743 0001534 96.4808 263.6594 15.05643685 06
| Epoch (UTC): | 25 May 2026 10:39:28 |
| Eccentricity: | 0.0001534 |
| inclination: | 97.4478° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.4743° |
| argument of perigee: | 96.4808° |
| revolutions per day: | 15.05643685 |
| mean anomaly at epoch: | 263.6594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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