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 53066U 26145.47595395 +.00000000 +00000-0 +30350-3 0 00002
2 53066 97.4475 325.4216 0001559 98.6643 261.4761 15.05657190 03
| Epoch (UTC): | 25 May 2026 11:25:22 |
| Eccentricity: | 0.0001559 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.4216° |
| argument of perigee: | 98.6643° |
| revolutions per day: | 15.05657190 |
| mean anomaly at epoch: | 261.4761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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