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 62930U 26145.13312999 +.00000000 +00000-0 +20681-3 0 00008
2 62930 97.9298 198.0232 0001617 281.8813 78.2215 14.75598202 05
| Epoch (UTC): | 25 May 2026 03:11:42 |
| Eccentricity: | 0.0001617 |
| inclination: | 97.9298° |
| perigee height: | 642 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 198.0232° |
| argument of perigee: | 281.8813° |
| revolutions per day: | 14.75598202 |
| mean anomaly at epoch: | 78.2215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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