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 26128.08689132 +.00000000 +00000-0 +18750-3 0 00003
2 25733 98.6839 172.3821 0012994 296.3218 63.6623 14.18908446 06
| Epoch (UTC): | 08 May 2026 02:05:07 |
| Eccentricity: | 0.0012994 |
| inclination: | 98.6839° |
| perigee height: | 820 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 172.3821° |
| argument of perigee: | 296.3218° |
| revolutions per day: | 14.18908446 |
| mean anomaly at epoch: | 63.6623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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