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 53073U 26145.47536499 +.00000000 +00000-0 +46483-3 0 00004
2 53073 97.6369 334.6685 0004504 328.2030 31.8933 15.22051141 05
| Epoch (UTC): | 25 May 2026 11:24:31 |
| Eccentricity: | 0.0004504 |
| inclination: | 97.6369° |
| perigee height: | 497 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 334.6685° |
| argument of perigee: | 328.2030° |
| revolutions per day: | 15.22051141 |
| mean anomaly at epoch: | 31.8933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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