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 60103U 26145.43078387 +.00000000 +00000-0 +30087-3 0 00002
2 60103 53.1601 40.8270 0001463 108.7876 251.3284 15.30121706 01
| Epoch (UTC): | 25 May 2026 10:20:19 |
| Eccentricity: | 0.0001463 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.8270° |
| argument of perigee: | 108.7876° |
| revolutions per day: | 15.30121706 |
| mean anomaly at epoch: | 251.3284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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