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 20253U 26141.97256774 +.00000000 +00000-0 +00000-0 0 00006
2 20253 12.4289 351.3234 0006149 29.2081 334.8725 1.00267597 02
| Epoch (UTC): | 21 May 2026 23:20:29 |
| Eccentricity: | 0.0006149 |
| inclination: | 12.4289° |
| perigee height: | 35762 km |
| apogee height: | 35814 km |
| right ascension of ascending node: | 351.3234° |
| argument of perigee: | 29.2081° |
| revolutions per day: | 1.00267597 |
| mean anomaly at epoch: | 334.8725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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