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 62387U 26145.01174125 +.00000000 +00000-0 +71173-3 0 00000
2 62387 44.9920 20.0515 0007616 176.9482 183.1458 15.50941763 07
| Epoch (UTC): | 25 May 2026 00:16:54 |
| Eccentricity: | 0.0007616 |
| inclination: | 44.9920° |
| perigee height: | 409 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 20.0515° |
| argument of perigee: | 176.9482° |
| revolutions per day: | 15.50941763 |
| mean anomaly at epoch: | 183.1458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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