▸Orbital parameters

Orbit class	SSO
Inclination	97.4298°
Eccentricity	0.0018092
Period	95.7 min
Apogee	564 km
Perigee	539 km
Mean motion	15.05073711 rev/day
RAAN	344.8389°
Arg of perigee	30.2814°
Mean anomaly	329.9454°
B*	1.9609e-4
Rev at epoch	48,967

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 42829U 17042E 26187.92920498 .00002738 00000-0 19609-3 0 9994

2 42829 97.4298 344.8389 0018092 30.2814 329.9454 15.05073711489673

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TECHNOSAT",
  "OBJECT_ID": "2017-042E",
  "EPOCH": "2026-07-06T22:18:03.31+00:00",
  "MEAN_MOTION": 15.05073711,
  "ECCENTRICITY": 0.0018092,
  "INCLINATION": 97.4298,
  "RA_OF_ASC_NODE": 344.8389,
  "ARG_OF_PERICENTER": 30.2814,
  "MEAN_ANOMALY": 329.9454,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 42829,
  "REV_AT_EPOCH": 48967,
  "BSTAR": 0.00019609,
  "MEAN_MOTION_DOT": 0.00002738,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	TECHNOSAT
Operator	Technical University of BerlinHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Germany
Launch date	Jul 14, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	18HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/42829

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.