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 58044U 26145.49210296 +.00000000 +00000-0 +15279-2 0 00001
2 58044 53.1610 171.2570 0001025 72.8240 287.2874 15.34120890 04
| Epoch (UTC): | 25 May 2026 11:48:37 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1610° |
| perigee height: | 463 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 171.2570° |
| argument of perigee: | 72.8240° |
| revolutions per day: | 15.34120890 |
| mean anomaly at epoch: | 287.2874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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