▸Orbital parameters

Orbit class	LEO
Inclination	55.0004°
Eccentricity	0.0010720
Period	92.7 min
Apogee	414 km
Perigee	399 km
Mean motion	15.53436963 rev/day
RAAN	213.1635°
Arg of perigee	349.9934°
Mean anomaly	10.0886°
B*	1.3920e-4
Rev at epoch	432

▸Two-line element set (TLE)

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

1 69472U 26128A 26188.08837516 .00008517 00000-0 13920-3 0 9999

2 69472 55.0004 213.1635 0010720 349.9934 10.0886 15.53436963 4323

▸ source OMM (JSON)

{
  "OBJECT_NAME": "DTC TEST OBJECT A",
  "OBJECT_ID": "2026-128A",
  "EPOCH": "2026-07-07T02:07:15.614+00:00",
  "MEAN_MOTION": 15.53436963,
  "ECCENTRICITY": 0.001072,
  "INCLINATION": 55.0004,
  "RA_OF_ASC_NODE": 213.1635,
  "ARG_OF_PERICENTER": 349.9934,
  "MEAN_ANOMALY": 10.0886,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69472,
  "REV_AT_EPOCH": 432,
  "BSTAR": 0.0001392,
  "MEAN_MOTION_DOT": 0.00008517,
  "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	DTC TEST OBJECT A
Operator	Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	China
Launch date	Jun 9, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	300HIGHvia 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/69472

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