▸Orbital parameters

Orbit class	LEO
Inclination	51.6235°
Eccentricity	0.0004381
Period	91.8 min
Apogee	368 km
Perigee	362 km
Mean motion	15.67864085 rev/day
RAAN	195.5907°
Arg of perigee	301.2245°
Mean anomaly	58.8321°
B*	8.2706e-4
Rev at epoch	2,329

▸Two-line element set (TLE)

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

1 67686U 98067YC 26187.24980961 .00093532 00000-0 82706-3 0 9994

2 67686 51.6235 195.5907 0004381 301.2245 58.8321 15.67864085 23299

▸ source OMM (JSON)

{
  "OBJECT_NAME": "UITMSAT-2",
  "OBJECT_ID": "1998-067YC",
  "EPOCH": "2026-07-06T05:59:43.55+00:00",
  "MEAN_MOTION": 15.67864085,
  "ECCENTRICITY": 0.00043812,
  "INCLINATION": 51.6235,
  "RA_OF_ASC_NODE": 195.5907,
  "ARG_OF_PERICENTER": 301.2245,
  "MEAN_ANOMALY": 58.8321,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67686,
  "REV_AT_EPOCH": 2329,
  "BSTAR": 0.00082705988,
  "MEAN_MOTION_DOT": 0.00093532,
  "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	UITMSAT-2
Operator	MARA University of TechnologyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Malaysia
Launch date	Oct 26, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1HIGHvia 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/67686

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