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 51284U 26145.45840779 +.00000000 +00000-0 +60444-4 0 00007
2 51284 97.8102 153.2015 0001614 90.3582 269.7820 14.88426091 02
| Epoch (UTC): | 25 May 2026 11:00:06 |
| Eccentricity: | 0.0001614 |
| inclination: | 97.8102° |
| perigee height: | 602 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 153.2015° |
| argument of perigee: | 90.3582° |
| revolutions per day: | 14.88426091 |
| mean anomaly at epoch: | 269.7820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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