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 62988U 26145.35976962 +.00000000 +00000-0 +15108-2 0 00008
2 62988 43.0007 259.0434 0001587 269.0825 90.9860 15.70913607 00
| Epoch (UTC): | 25 May 2026 08:38:04 |
| Eccentricity: | 0.0001587 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 259.0434° |
| argument of perigee: | 269.0825° |
| revolutions per day: | 15.70913607 |
| mean anomaly at epoch: | 90.9860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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