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 53198U 26145.61718225 +.00000000 +00000-0 +59854-4 0 00004
2 53198 97.4446 205.6113 0001730 182.5793 177.5425 15.05663824 07
| Epoch (UTC): | 25 May 2026 14:48:44 |
| Eccentricity: | 0.0001730 |
| inclination: | 97.4446° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.6113° |
| argument of perigee: | 182.5793° |
| revolutions per day: | 15.05663824 |
| mean anomaly at epoch: | 177.5425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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