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 53233U 26145.39841682 +.00000000 +00000-0 -39547-4 0 00001
2 53233 97.4511 205.3167 0001661 144.3443 215.7896 15.05652374 02
| Epoch (UTC): | 25 May 2026 09:33:43 |
| Eccentricity: | 0.0001661 |
| inclination: | 97.4511° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.3167° |
| argument of perigee: | 144.3443° |
| revolutions per day: | 15.05652374 |
| mean anomaly at epoch: | 215.7896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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