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 42945U 26145.48660447 +.00000000 +00000-0 +14250-3 0 00009
2 42945 34.9959 167.6980 0002603 298.3356 61.7090 15.02977348 08
| Epoch (UTC): | 25 May 2026 11:40:42 |
| Eccentricity: | 0.0002603 |
| inclination: | 34.9959° |
| perigee height: | 556 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 167.6980° |
| argument of perigee: | 298.3356° |
| revolutions per day: | 15.02977348 |
| mean anomaly at epoch: | 61.7090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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