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 53505U 26145.33667103 +.00000000 +00000-0 +48697-3 0 00005
2 53505 97.6049 274.0980 0002095 253.8473 106.2560 15.74488527 04
| Epoch (UTC): | 25 May 2026 08:04:48 |
| Eccentricity: | 0.0002095 |
| inclination: | 97.6049° |
| perigee height: | 345 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 274.0980° |
| argument of perigee: | 253.8473° |
| revolutions per day: | 15.74488527 |
| mean anomaly at epoch: | 106.2560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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