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 68707U 26145.12798242 +.00000000 +00000-0 +68315-3 0 00000
2 68707 53.1597 39.9320 0001114 93.6453 266.4684 15.49344478 08
| Epoch (UTC): | 25 May 2026 03:04:17 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1597° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 39.9320° |
| argument of perigee: | 93.6453° |
| revolutions per day: | 15.49344478 |
| mean anomaly at epoch: | 266.4684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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