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 45198U 26145.58335647 +.00000000 +00000-0 +23436-3 0 00000
2 45198 53.0428 359.6160 0000562 94.6005 83.4312 15.62507424 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000562 |
| inclination: | 53.0428° |
| perigee height: | 380 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 359.6160° |
| argument of perigee: | 94.6005° |
| revolutions per day: | 15.62507424 |
| mean anomaly at epoch: | 83.4312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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