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 51949U 26145.59285581 +.00000000 +00000-0 +75647-3 0 00004
2 51949 63.4573 348.5254 0122216 355.9806 4.0312 15.17975187 00
| Epoch (UTC): | 25 May 2026 14:13:42 |
| Eccentricity: | 0.0122216 |
| inclination: | 63.4573° |
| perigee height: | 428 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 348.5254° |
| argument of perigee: | 355.9806° |
| revolutions per day: | 15.17975187 |
| mean anomaly at epoch: | 4.0312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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