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 63121U 26145.46013213 +.00000000 +00000-0 +66295-3 0 00005
2 63121 42.9989 298.7210 0001221 279.1355 80.9358 15.27592689 00
| Epoch (UTC): | 25 May 2026 11:02:35 |
| Eccentricity: | 0.0001221 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 298.7210° |
| argument of perigee: | 279.1355° |
| revolutions per day: | 15.27592689 |
| mean anomaly at epoch: | 80.9358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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