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 25544U 26038.50283897 +.00000000 +00000-0 +23050-3 0 00007
2 25544 51.6315 221.5822 0011000 74.6214 285.5989 15.48462076 00
| Epoch (UTC): | 07 February 2026 12:04:05 |
| Eccentricity: | 0.0011000 |
| inclination: | 51.6315° |
| perigee height: | 414 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 221.5822° |
| argument of perigee: | 74.6214° |
| revolutions per day: | 15.48462076 |
| mean anomaly at epoch: | 285.5989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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