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 62998U 26145.19902201 +.00000000 +00000-0 +72902-3 0 00002
2 62998 42.9981 71.4824 0001163 209.6908 150.3878 15.27562300 03
| Epoch (UTC): | 25 May 2026 04:46:35 |
| Eccentricity: | 0.0001163 |
| inclination: | 42.9981° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.4824° |
| argument of perigee: | 209.6908° |
| revolutions per day: | 15.27562300 |
| mean anomaly at epoch: | 150.3878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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