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 53973U 26145.26197032 +.00000000 +00000-0 +82460-4 0 00002
2 53973 53.2154 240.2537 0001595 85.1331 274.9844 15.08843222 06
| Epoch (UTC): | 25 May 2026 06:17:14 |
| Eccentricity: | 0.0001595 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 240.2537° |
| argument of perigee: | 85.1331° |
| revolutions per day: | 15.08843222 |
| mean anomaly at epoch: | 274.9844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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