▸Orbital parameters

Orbit class	SSO
Inclination	97.7317°
Eccentricity	0.0000644
Period	96.5 min
Apogee	590 km
Perigee	589 km
Mean motion	14.92615094 rev/day
RAAN	84.3797°
Arg of perigee	103.3914°
Mean anomaly	256.7377°
B*	1.0772e-4
Rev at epoch	954

▸Two-line element set (TLE)

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

1 68994U 26100Q 26187.22615593 .00001053 00000-0 10772-3 0 9991

2 68994 97.7317 84.3797 0000644 103.3914 256.7377 14.92615094 9541

▸ source OMM (JSON)

{
  "OBJECT_NAME": "NULINK-2",
  "OBJECT_ID": "2026-100Q",
  "EPOCH": "2026-07-06T05:25:39.872+00:00",
  "MEAN_MOTION": 14.92615094,
  "ECCENTRICITY": 0.0000644,
  "INCLINATION": 97.7317,
  "RA_OF_ASC_NODE": 84.3797,
  "ARG_OF_PERICENTER": 103.3914,
  "MEAN_ANOMALY": 256.7377,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68994,
  "REV_AT_EPOCH": 954,
  "BSTAR": 0.00010772,
  "MEAN_MOTION_DOT": 0.00001053,
  "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	NULINK-2
Operator	NuSpace Pte Ltd.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Singapore
Launch date	May 3, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3HIGHvia 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/68994

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