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 53445U 26145.63763936 +.00000000 +00000-0 +65725-3 0 00003
2 53445 97.5563 273.6907 0003438 106.9843 253.1792 15.63291926 04
| Epoch (UTC): | 25 May 2026 15:18:12 |
| Eccentricity: | 0.0003438 |
| inclination: | 97.5563° |
| perigee height: | 376 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 273.6907° |
| argument of perigee: | 106.9843° |
| revolutions per day: | 15.63291926 |
| mean anomaly at epoch: | 253.1792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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