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 62700U 26145.20531163 +.00000000 +00000-0 +23835-3 0 00001
2 62700 97.7065 225.0689 0002811 100.3700 259.7838 14.96576204 02
| Epoch (UTC): | 25 May 2026 04:55:38 |
| Eccentricity: | 0.0002811 |
| inclination: | 97.7065° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 225.0689° |
| argument of perigee: | 100.3700° |
| revolutions per day: | 14.96576204 |
| mean anomaly at epoch: | 259.7838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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