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 62115U 26145.47037477 +.00000000 +00000-0 +52860-3 0 00009
2 62115 42.9964 62.3907 0001155 268.0953 91.9766 15.27595163 05
| Epoch (UTC): | 25 May 2026 11:17:20 |
| Eccentricity: | 0.0001155 |
| inclination: | 42.9964° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.3907° |
| argument of perigee: | 268.0953° |
| revolutions per day: | 15.27595163 |
| mean anomaly at epoch: | 91.9766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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