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 53691U 26145.63652720 +.00000000 +00000-0 +91694-5 0 00000
2 53691 97.4492 26.6651 0002730 97.3819 262.7718 15.05658667 08
| Epoch (UTC): | 25 May 2026 15:16:35 |
| Eccentricity: | 0.0002730 |
| inclination: | 97.4492° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.6651° |
| argument of perigee: | 97.3819° |
| revolutions per day: | 15.05658667 |
| mean anomaly at epoch: | 262.7718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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