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 61215U 26145.56798568 +.00000000 +00000-0 +26954-4 0 00000
2 61215 53.1610 325.0132 0001185 90.4803 269.6333 15.30193814 05
| Epoch (UTC): | 25 May 2026 13:37:53 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 325.0132° |
| argument of perigee: | 90.4803° |
| revolutions per day: | 15.30193814 |
| mean anomaly at epoch: | 269.6333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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