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 62308U 26145.39178240 +.00000000 +00000-0 +30403-3 0 00007
2 62308 53.1576 197.9077 0000937 95.8786 264.2321 15.30206382 00
| Epoch (UTC): | 25 May 2026 09:24:09 |
| Eccentricity: | 0.0000937 |
| inclination: | 53.1576° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 197.9077° |
| argument of perigee: | 95.8786° |
| revolutions per day: | 15.30206382 |
| mean anomaly at epoch: | 264.2321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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