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 25733U 26135.13851999 +.00000000 +00000-0 +14875-3 0 00003
2 25733 98.6833 179.2913 0012966 273.8840 86.0853 14.18912964 02
| Epoch (UTC): | 15 May 2026 03:19:28 |
| Eccentricity: | 0.0012966 |
| inclination: | 98.6833° |
| perigee height: | 820 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 179.2913° |
| argument of perigee: | 273.8840° |
| revolutions per day: | 14.18912964 |
| mean anomaly at epoch: | 86.0853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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