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 65136U 26145.52368494 +.00000000 +00000-0 +27999-3 0 00002
2 65136 51.9002 180.9620 0000271 64.8214 295.2776 14.79940027 02
| Epoch (UTC): | 25 May 2026 12:34:06 |
| Eccentricity: | 0.0000271 |
| inclination: | 51.9002° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 180.9620° |
| argument of perigee: | 64.8214° |
| revolutions per day: | 14.79940027 |
| mean anomaly at epoch: | 295.2776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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