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 48000U 26145.25692463 +.00000000 +00000-0 +12371-2 0 00006
2 48000 53.1282 243.5127 0003832 316.8149 43.2554 15.40082427 03
| Epoch (UTC): | 25 May 2026 06:09:58 |
| Eccentricity: | 0.0003832 |
| inclination: | 53.1282° |
| perigee height: | 443 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 243.5127° |
| argument of perigee: | 316.8149° |
| revolutions per day: | 15.40082427 |
| mean anomaly at epoch: | 43.2554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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