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 51102U 26145.58511021 +.00000000 +00000-0 +78502-4 0 00009
2 51102 98.4565 166.0782 0603539 258.1436 95.1485 14.20281925 09
| Epoch (UTC): | 25 May 2026 14:02:33 |
| Eccentricity: | 0.0603539 |
| inclination: | 98.4565° |
| perigee height: | 390 km |
| apogee height: | 1259 km |
| right ascension of ascending node: | 166.0782° |
| argument of perigee: | 258.1436° |
| revolutions per day: | 14.20281925 |
| mean anomaly at epoch: | 95.1485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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